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 2015 March 20 Total Solar Eclipse from a B737 business jet
 leaving Paris-Le Bourget (LBG-LFPB), France

2015 Eclipse Flight Partnership Longtail Aviation
 In partnership with

The point of greatest eclipse (totality phase during 2 min 46 sec) was located in the middle of the North Atlantic Ocean east of Iceland and northwest of the Faroe Islands. As weather prospects weren’t that great for the few ground-based locations, seeing it from the stratosphere was tantalizing. Svalbard was the second choice as there are quite a few clear days at that time of the year, and the fact is the sky was indeed clear on eclipse day. The Faroe Islands were the third choice as the weather there changes very quickly which is why some saw it and others didn’t.
To observe the 2015 March 20 total solar eclipse, I am offering very special eclipse flights at the edge of the stratosphere (see the similar flight executed in November 2013) in partnership with AmJet Executive and Dassault Falcon Service, but also a more conventional, and nevertheless exceptionnal, flight using a private B737-700 business jet in partnership with Longtail Aviation. Those interested in this latest eclipse flight should contact me ASAP by clicking on the "Inquiry & Booking" mauve button below.

You can use this solar eclipse calculator to compute the local circumstances of the eclipse, and the solar eclipse timer notifies the beginning of the various events. A time exposure calculator is there to help you choose your camera settings.

Click on thumbnails for a larger version

Tours (very limited space)
Stratospheric Eclipse Flight :
North Atlantic
[ Book Now 4th Aircraft ]

Norway :
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Arctic Expedition :
North Pole
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The Luxury Eclipse Flight Not To Be Missed
Full charter at 80,000€ or 4,000€ per seat (up to two windows)
Additional costs to include relocation of the aircraft may be added
Inquiry & Booking

Land-based observers in Svalbard will experience at most 2 minutes and 28 seconds of totality and about 6 seconds less in the Faroe islands, provided the weather is good enough. However, at 39,000 feet (11,888 meters), this eclipse flight will fly above potential cloud systems and add about a minute and twenty seconds of totality! Nevertheless this eclipse flight will be surpassed by the three private Falcon 7X operating at 49,000 feet (14,935 meters) in the lower stratosphere where the totality duration will be of at least 3 minutes and 50 seconds, and pushing the aircraft to its maximum speed (Mach 0.90) would bring up to four minutes. No other commercial or private flight will surpass that duration or the cruise altitude during this eclipse, and those three passenger flights will be the highest yet during a solar eclipse after the ones of the Concorde in 1973 and 1999. There is also an opportunity to give a wink to Don Connolly’s famous painting of the Concorde 001 and the black Sun, as those three aircrafts will be flying 10,000 feet above you, and to the east, so you will see them streaking the dark sky near the eclipsed Sun surrounded by its corona.
Up to 26 spaces, out of the 27 seats, will be sold on this exceptionnal flight, so hurry up to reserve yours. The B737-700 business jet will be operated by our Bermuda-based partner Longtail Aviation.

Use of this simulation is strictly forbidden without my written approval. All commercial uses are subject to a fee for every planned flight.

Total Solar Eclipse 2015 North Atlantic Ocean Eclipse Flight B737-700
Boeing 737-700 business aircraft to be used for the eclipse flight over the North Atlantic Ocean
(the winglet is out of the way of the Sun from all the windows)
Boeing 737-700 NG Dimension Chart
The winglet will be out of the way of the Sun from all the windows

Boeing 737-700 NG Window Metrology
The windows are all identical in size and shape: 25 centimeters (9.8") wide by 34 centimeters (13.4") high. The inter-window spacing is 50 centimeters (19.7"), and we have 94 centimeters (37") between the center of the windows and the floor.

Flight Planning

Total Solar Eclipse 2008 Arctic Flight Dan McGlaun
TSE 2008 eclipse flight over the Arctic (courtesy of Dan McGlaun)
The preliminary version of this 5-hour eclipse flight plan was developed to optimize the quality of the observations, in duration, sky darkness and transparency, while minimizing to near-zero risks that are otherwise high-probability at ground-based locations (Faroe Islands, Svalbard or North Pole). The nominal flight plan is built around an eclipse-viewing Totality Run (TR) constrained by celestial mechanics, aircraft operational considerations, and a need to maintain in situ flexibility to implement contingency alternatives. For baseline planning and logistical purposes we build from:
  • a flight altitude for eclipse-viewing of 39,000 feet AMSL,
  • a nominal ground speed of 445 knots (Mach 0.78),
  • no wind (so ground speed equal to air speed, and heading equal to course).
Detailed pre-eclipse flight planning, and in-flight execution, will incorporate and allow for the full range of possible flight levels, air speeds, and wind-vectors that may be encountered in flight to re-optimize the Totality Run in situ as may be necessary or desired.
We define the baseline Totality Run such that the aircraft is centrally located at the apex of the lunar umbral shadow (but corrected for the irregular lunar limb profile) at the topocentric instants of Maximum Eclipse at the chosen intercept point. We also define the baseline Totality Run so that the aircraft velocity vector at mid-eclipse places the Sun perpendicularly to the right-side windows of the aircraft passenger cabin to provide optimum out-the-window viewing and utilization. This orientation also provides an optimal orientation to prolong the duration of totality to a theoretical maximum anywhere along the path of totality by using the aircraft’s speed to partially keep pace with the lunar shadow. With these constraints, we compute, and tabulate below, three key time correlated waypoints for the totality runs that define the lunar shadow intercept and crossing by the aircraft designated C2 (eclipse second contact), MAX (corresponding to the UTC instant of maximum eclipse), and C3 (eclipse third contact). MAX, in both time and position, will depend upon the aircraft altitude AMSL. C2 and C3 will also depend upon the aircraft ground speed and track (i.e., airspeed and winds aloft).
The earlier start of the pre-totality outbound leg of the Totality Run is to be defined by a pre-totality time-correlated waypoint fourteen minutes before mid-eclipse. The aircraft is initially positioned on the MAX-eclipse intercept track at the requisite course/heading, distance, and flight-time from the intercept point allowing for airspeed adjustment in the run up to the C2 time-correlated waypoint to compensate for deviations due to actual versus predicted winds aloft (holding the MAX intercept time-correlated waypoint invariant). After C3 the aircraft will remain on the MAX-to-C3 heading for six minutes following mid-eclipse to allow viewing of the recession of the Moon’s shadow before returning back to Paris.
The baseline flight plan presented here is of sufficient fidelity for the presumed nominal parametric conditions assumed that, if rigorously followed, will successfully result in a highly viewing-optimized and geometrically precise time-correlated mid-eclipse intercept with the aircraft concentrically located along the apex of the lunar umbral shadow cone.
However, all timings and correlated locations, and maps presented here are valid only for the specific set of baseline assumptions used here and shouldn’t be used elsewhere. Later recomputation of the eclipse observation plan (and thus to a small degree end-to-end) flight plan, is expected and anticipated.
The Totality Run (TR) is entered nominally at the completion of a heading re-alignment maneuver with a constant radius turn onto the TR track at the requisite UTC time, location, altitude, TAS, and heading. Once on the TR track, before the start of totality at C2, small adjustments to the aircraft speed may be made to compensate for winds-aloft or turn-exit navigation errors to maintain the desired mid-eclipse flight profile.

Baseline Flight Plan

Time-Correlated Waypoints and Eclipse Circumstances
Flight scenario: totality run at FL 390, Mach 0.78 (TAS 445 kt). Outbound and inbound legs at FL 370, Mach 0.78 (TAS 445 kt).
(details subject to change)

## Flight Plan: Phase/Description (Paris) UTC Time
Leg Time Flight
  Sunrise at Paris-Le Bourget airport
Moonrise is about 5 minutes before
05:53 48.954501° N 2.433107° E   89.3
  Boarding the aircraft 06:30 48.954501° N 2.433107° E  
01 Take-off from Paris-Le Bourget airport 07:07:52 48.954501° N 2.433107° E 336.8   11.3 103.5
02 Climb to FL 370   127.5 17m 12s  
03 Start Outbound Cruise 07:25:04 50.900986° N 1.125726° E 335.8   FL 370  
04  Outbound Cruise
 (with 20 mins contingency buffer)
At pilot’s discretion / direction in response to in situ conditions 637.5 1h 35m 53s  
05  1st Contact (C1) 08:30   17.4 118.2
06  Climb to FL 390 09:11:01 60.289246° N 7.587097° W 328.6 127.5 17m 12s  
07 End Outbound Cruise
Start Pre-TR Constant Radius Right Turn
09:28:13 62.074849° N 9.936729° W   FL 390  
08 105.2° Constant Radius Right Turn
25° bank, 6.2 NM radius
  62.131595° N 9.753700° W   11.4 1m 32s FL 390  
09 Totality Run Start
(Mid-Eclipse - 14 mins)
Mach 0.78
09:29:45 62.199551° N 9.918757° W 41.3   FL 390 17.5 127.3
10  Waning Solar Crescent Viewing
 Lights inside the cabin are switched off
  88.4 12m 03s FL 390  
11 2nd Contact (C2) 09:41:51 63.304278° N 7.729417° W 43.2   FL 390 18.6 132.7
12  Totality   14.1 1m 54s FL 390  
13   Mid-Eclipse 09:43:45 63.471107° N 7.377786° W 43.6   FL 390 18.8 133.6
14  Totality   13.7 1m 51s FL 390  
15 3rd Contact (C3) 09:45:36 63.638528° N 7.018833° W 44.9   FL 390 18.9 134.4
16  Waxing Solar Crescent Viewing
 Lights inside the cabin are switched on
  30.8 4m 09s FL 390  
17 Totality Run End
(Mid-Eclipse + 6 mins)
Mach 0.78
09:49:45 64.001333° N 6.219388° W 44.6   FL 390 19.2 136.3
18 118.2° Constant Radius Right Turn
25° bank, 6.2 NM radius
  63.933386° N 6.043818° W   12.8 1m 43s FL 390  
19 Start Inbound Cruise at 445 kt 09:51:28 63.969410° N 5.824828° W 159.5   FL 390  
20  Descent to FL 370   117.9 17m 37s  
21  Inbound Cruise 10:07:22 62.129970° N 4.361127° W 160.8 707.5 1h 35m 22s FL 370  
22  4th Contact (C4) 10:47   30.0 155.1
23 End Inbound Cruise
Start Final Descent
11:42:46 50.866404° N 1.734358° E   FL 370  
24 Descent from FL 370   117.9 15m 54s  
25 Landing at Paris-Le Bourget airport 11:58:39 48.954501° N 2.433107° E   40.9 180.3
Total Time and Distance



4h 50m 47s

  Notes: (1) Totality run to place the Sun "straight out" the main cabin windows at mid-eclipse.
(2) No statistical (i.e., anticipated seasonal average) wind vectors have (yet) been assumed.
(3) Constant radius turns onto/off the TR track assume a bank angle (and thus derived turn radius/duration) of 25°.
(4) Ascent and Descent profiled durations and ground-track distances are to-be-verified.
(5) Geodetic coordinate reference frame is WGS84.
(6) ΔT: 67.8 seconds (current IERS derived prediction for March 2015).
(7) Local time in Paris is UTC+1, that is 8:07am for take-off and 12:58pm for landing.

TSE 2015 March 20 Dassault Falcon 7X Baseline Eclipse Flight Path
TSE 2015 March 20 End-to-end baseline flight path from/to Paris-Le Bourget airport
(the totality path is shown at sea level)

The end-to-end, from take-off to landing, flight planning seamlessly merges into the immutable, but nevertheless tunable based on actual flight conditions, Totality Run (TR). Most critical is entering the pre-planned Totality Run exactly as specified with minimal error. Any delay and the Moon’s shadow will pass over the location where the aircraft should have been and totality will be missed. This must, and will be, be avoided with the following measures:
  • To mitigate against the operational possibilities of a "time-critical" take-off delay from LBG for any reason, an earlier than time-critical wheels-up time for a central intercept at the chosen mid-eclipse intercept point is planned. This is 10 minutes. Choosing a private airport does help somewhat to reduce those potential delays.
  • The climb phase of the flight must be defined in detail by the aircraft flight planners and air traffic can have an impact. For initial planning we have an estimated climb to FL 370 consuming 24 minutes of time and covering 156 nautical miles.
  • A "most economical" TAS cruise speed of Mach 0.78 is used for initial planning. This, importantly, provides some leverage to invoke higher or lower cruise speeds, within performance limits, to allow mitigation against unfavorable head or tail winds that would otherwise result in a too-late or too-early arrival at the TR start point, or during time/position decorrelation during the TR itself. Performance options that may be invoked are to be discussed with the flight crew and operations planners.
  • In the event of an on-schedule earlier than time-critical, take-off, the "extra" time programmed into the flight plan to otherwise compensate for a delay must be consumed by either maneuvering enroute (executing a loop for example), and/or flying at a slower TAS to the time-critical TR start point. This is a detail of the flight planning that will necessarily worked in concert with the flight crew and flight planners (given airspace and other operational constraints) at a later date closer to eclipse time. Implementation details will be worked later in the final planning with the pilot in command and flight planners.
    Repositioning the heading re-alignment maneuver following the outbound cruise phase can be done in situ using my Solar Eclipse Maestro E-Flight eclipse flight optimization and navigation software.
Lets now see why this intercept location was chosen. The track, geometry, and location of the path of totality, and the time-correlated UTCs of key eclipse events (e.g., start, end, and middle of totality) that ultimately constrain an end-to-end eclipse-observation flight plan, as seen from a moving aircraft, will depend in detail on the aircraft altitude above mean sea level and its velocity vector (ground speed and direction) as modified by winds aloft. Baseline (Phase 1) eclipse-flight planning, as discussed and presented here, makes assumptions for later (Phase 2) optimization and refinement within constrained margins with dependencies on in situ conditions that may be parametrized in final computations. A baseline flight plan is developed to provide a framework to be refined for an executable flight mission subject to refinements and constraints levied by aircraft performance and operations factors. Phase 2 "fine tuning" of the flight plan (e.g., in light of statistically anticipated and actual winds aloft) is later expected.
We designate a "Totality Run" (TR) as the portion of the flight devoted to the observation of the total phase of the solar eclipse. The Totality Run is planned so the aircraft has assumed straight-and-level flight at constant speed at and throughout the totality and during pre/post flanking intervals closely prior to and after totality.
The point (time correlated location and UTC) of "Mid-Eclipse" (ME) intercept is the instant at which the aircraft is concentrically located in the Moon’s umbral shadow. The Totality Run is planned so the aircraft heading is the solar azimuth at mid-eclipse minus 90 degrees, so the Sun will present itself "straight out" to the sun-side passenger windows. This is the right (starboard) side of the aircraft, so enabling an aircraft velocity vector component in the velocity vector of the Moon’s shadow with a resulting increase in the duration of totality as seen from the moving aircraft. All this leads to select a location where the Moon’s umbral shadow velocity is the lowest (see graphs below), that is generally close to the middle of the totality path, to prolong totality with an aircraft moving in the direction of the lunar velocity vector.
TSE 2015 Moon Umbral Shadow Velocity UTC Time 49000 37000 Feet Sea Level
TSE 2015 Moon’s umbral shadow velocity over a one hour window centered on the chosen mid-intercept time

One can notice how fast the Moon’s umbral shadow is moving, even at its lowest speed. No current commercial aircraft can match this speed of about 3,200 kph (1,988 mph). The Concorde 001 in June 1973 is the only aircraft in history that managed to briefly keep up with it.
TSE 2015 Moon Umbral Shadow Velocity UTC Time 49000 37000 Feet Sea Level
TSE 2015 Moon’s umbral shadow velocity over an 8-minute window where it’s the lowest

The detailed graph shows that the Moon’s umbral shadow velocity changes with altitude, which is why it has to be computed for the specific altitude of the eclipse flight.
In practice, small compensating adjustments to the derived Totality Run (and pre-totality run flight plan) are made based upon:
  • statistically most-likely, and/or in situ actual winds-aloft,
  • different TAS during the Totality Run within operating limits,
  • different flight level to the limit of the service ceiling with trade of achievable ground speed.
Such parametrically defined variations to the baseline flight plan, subject to aircraft operational and performance constraints, will be reviewed and discussed with the aircraft flight operations and planning personnel, and are readily (re)-computatble as needed with my Solar Eclipse Maestro E-Flight eclipse flight optimization and navigation software.

TSE 2015 Moon Umbral Shadow Apex Location Shift UTC Time 49000 37000 Feet Sea Level
TSE 2015 Moon’s umbral shadow apex location shift depending on the altitude and time (with reference to sea level)

The time-correlated position (centerline track) of the Moon’s umbral shadow shifts in latitude and longitude with topocentric altitude AMSL. This graph shows the difference in centerline topographic coordinates at 37,000 and 49,000 feet (11,278 and 14,935 meters) compared to sea level over the time.
One can see again that the choice of an intercept at 09:43:45 UTC is completely justified.

Preview of the Baily’s Beads

Baily’s beads at second contact from the aircraft at 39,000 feet (11,888 meters) over the North Atlantic Ocean

Baily’s beads at second and third contacts from the aircraft at 39,000 feet (11,888 meters) over the North Atlantic Ocean

Baily’s beads at third contact from the aircraft at 39,000 feet (11,888 meters) over the North Atlantic Ocean

From the height of our private Boeing 737-700, the apparent horizon is 389 kilometers away and is depressed by 3.5 degrees with respect to the astronomical horizon. Looking straight out on the Sun-side windows to the southeast at an azimuth of 133.6 degrees from true north, the black Sun will stand 22.3 degrees above the apparent horizon and 18.8 degrees above the astronomical horizon.
From the aircraft you’ll clearly see the curvature of the Earth and the Moon’s umbral shadow extending near to the horizon with the Faroe Islands on the right-hand side.
Stars brighter than visual magnitude +3.5 are shown where they will appear in the sky at mid-totality. The planets Mercury, Venus and Mars should all be visible as well along the Ecliptic. Venus will be visible to the naked eye several minutes before totality, Mercury likely shortly before totality and Mars barely discernable during totality.
Although seeing northern lights during totality has never been reported, we do have a slight chance during this eclipse flight as the Sun’s solar cycle is still near its maximum and the auroral oval usually passes just north of our location when the conditions are right.
TSE 2015 March 20 Boeing 737-700 Flight Sky Mid-Totality Star Magnitude 3.5
TSE 2015 March 20 sky at mid-totality (09:43:45 UTC) from our Boeing 737-700 at 39,000 feet (11,888 meters)
[the view will be very similar to this image taken from the other stratospheric eclipse flights]

Animation of the Moon’s umbral shadow from the aircraft at 39,000 feet (11,888 meters) over the North Atlantic Ocean

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Last page update on December 20, 2013.
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