STARLINK-35902, 66626
Orbit data source: Space-Track
STARLINK-35902, 66626 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 23 Nov 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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66626 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 17.7 m
Radar Cross Section
41.120 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 STARLINK-35902
1 66626U 25271K 26264.39981013 .00019317 00000-0 58117-3 0 9993
2 66626 53.1585 309.2658 0001305 71.3583 288.7562 15.34410305 47559Epoch: 2026-09-21T09:35Z
TLE epoch observation values (Epoch: 2026-09-21T09:35:43.595Z)
Latitude
0.00006°
Longitude
165.05401°
Altitude
463.287 km
Speed
7.636 km/s
True Right ascension
20h 37m 03s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
17:12:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.822 km
Perigee altitude
462.037 km
Semi-major axis
6,841.067 km
Eccentricity
0.00013
Inclination
53.1585°
RAAN
309.2658°
Arg. of periapsis
71.3583°
True anomaly
288.74204°
Mean anomaly
288.7562°
Eccentric anomaly
288.74912°
Mean motion
3.83581 °/min
Orbital period
93.85 mins
BSTAR
0.00058117
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Other satellites on launch #271 in the year 2025 (2025-11-23 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.STARLINK-35902 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-23 05:33:48.464Z | 235.949° WSW | 2026-09-23 05:35:48.464Z | 283.103° WNW | 75.249° | 2026-09-23 05:38:48.464Z | 46.604° ENE |
| 4 mins | 2026-09-23 10:29:48.464Z | 344.041° N | 2026-09-23 10:31:48.464Z | 20.952° NNE | 17.223° | 2026-09-23 10:33:48.464Z | 58.212° ENE |
| 5 mins | 2026-09-23 12:07:48.464Z | 313.439° NW | 2026-09-23 12:09:48.464Z | 1.015° NNE | 79.913° | 2026-09-23 12:12:48.464Z | 127.442° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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