STARLINK-35622, 66103
Orbit data source: Space-Track
STARLINK-35622, 66103 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 19 Oct 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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66103 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 + 2 Pan, 17.7 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 STARLINK-35622
1 66103U 25236T 26170.78544710 .00003469 00000-0 11373-3 0 9996
2 66103 53.1601 349.1014 0001152 100.3729 259.7404 15.34404204 38589Epoch: 2026-06-19T18:51Z
TLE epoch observation values (Epoch: 2026-06-19T18:51:02.629Z)
Latitude
0.00002°
Longitude
158.33102°
Altitude
463.733 km
Speed
7.636 km/s
True Right ascension
23h 16m 24s
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
07:23:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.736 km
Perigee altitude
462.16 km
Semi-major axis
6,841.085 km
Eccentricity
0.00012
Inclination
53.1601°
RAAN
349.1014°
Arg. of periapsis
100.3729°
True anomaly
259.72741°
Mean anomaly
259.7404°
Eccentric anomaly
259.73391°
Mean motion
3.8358 °/min
Orbital period
93.85 mins
BSTAR
0.00011373
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Other satellites on launch #236 in the year 2025 (2025-10-19 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-35622 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 | 2026-06-20 21:57:12.227Z | 291.256° WNW | 2026-06-20 22:00:12.227Z | 209.267° SW | 31.625° | 2026-06-20 22:02:12.227Z | 163.475° S |
| 5 mins | 2026-06-21 14:50:12.227Z | 259.464° W | 2026-06-21 14:52:12.227Z | 309.886° NW | 34.262° | 2026-06-21 14:55:12.227Z | 34.923° NE |
| 4 mins | 2026-06-21 19:47:12.227Z | 354.398° N | 2026-06-21 19:48:12.227Z | 18.118° NNE | 21.507° | 2026-06-21 19:51:12.227Z | 79.685° E |
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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