STARLINK-35210, 65903
Orbit data source: Space-Track
STARLINK-35210, 65903 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 07 Oct 2025 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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65903 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
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 STARLINK-35210
1 65903U 25224X 26062.12173235 .00026857 00000-0 91641-3 0 9990
2 65903 53.1605 42.2109 0001540 71.4945 288.6223 15.30172416 23841Epoch: 2026-03-03T02:55Z
TLE epoch observation values (Epoch: 2026-03-03T02:55:17.675Z)
Latitude
0°
Longitude
-162.51808°
Altitude
475.86 km
Speed
7.629 km/s
True Right ascension
02h 48m 50s
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
17:48:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.609 km
Perigee altitude
474.498 km
Semi-major axis
6,853.691 km
Eccentricity
0.00015
Inclination
53.1605°
RAAN
42.2109°
Arg. of periapsis
71.4945°
True anomaly
288.60558°
Mean anomaly
288.6223°
Eccentric anomaly
288.61394°
Mean motion
3.82522 °/min
Orbital period
94.11 mins
BSTAR
0.00091641
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Other satellites on launch #224 in the year 2025 (2025-10-07 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-35210 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-04 01:01:59.635Z | 218.718° SW | 2026-03-04 01:04:59.635Z | 175.968° S | 40.899° | 2026-03-04 01:08:59.635Z | 55.105° ENE |
| 4 mins | 2026-03-04 02:41:59.635Z | 300.376° NW | 2026-03-04 02:43:59.635Z | 345.306° N | 19.696° | 2026-03-04 02:45:59.635Z | 21.804° NNE |
| 5 mins | 2026-03-04 07:37:59.635Z | 322.94° NNW | 2026-03-04 07:39:59.635Z | 7.472° NNE | 38.057° | 2026-03-04 07:42:59.635Z | 111.284° ESE |
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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