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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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational spacecraft
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 17.7 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 STARLINK-35210
1 65903U 25224X 25341.29809621 .00036657 00000-0 12431-2 0 9990
2 65903 53.1603 80.8520 0001416 85.1270 274.9893 15.30215365 10702Epoch: 2025-12-07T07:09Z
TLE epoch observation values (Epoch: 2025-12-07T07:09:15.512Z)
Latitude
0.00002°
Longitude
-102.77611°
Altitude
475.985 km
Speed
7.629 km/s
True Right ascension
05h 23m 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
22:43:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.396 km
Perigee altitude
474.455 km
Semi-major axis
6,853.563 km
Eccentricity
0.00014
Inclination
53.1603°
RAAN
80.852°
Arg. of periapsis
85.127°
True anomaly
274.97314°
Mean anomaly
274.9893°
Eccentric anomaly
274.98122°
Mean motion
3.82533 °/min
Orbital period
94.11 mins
BSTAR
0.0012431
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-08 08:23:13.227Z | 176.641° S | 2025-12-08 08:25:13.227Z | 140.963° SSE | 19.747° | 2025-12-08 08:28:13.227Z | 81.512° E |
| 5 mins | 2025-12-08 10:01:13.227Z | 261.528° W | 2025-12-08 10:03:13.227Z | 317.279° NNW | 34.686° | 2025-12-08 10:06:13.227Z | 35.566° NE |
| 5 mins | 2025-12-08 14:58:13.227Z | 342.325° N | 2025-12-08 15:00:13.227Z | 26.57° NE | 22.61° | 2025-12-08 15:03:13.227Z | 83.414° E |
| 5 mins | 2025-12-08 16:36:13.227Z | 291.808° WNW | 2025-12-08 16:38:13.227Z | 231.099° WSW | 37.385° | 2025-12-08 16:41:13.227Z | 151.831° SSE |
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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