STARLINK-35329, 65908
Orbit data source: Space-Track
STARLINK-35329, 65908 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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65908 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-35329
1 65908U 25224AC 25340.67438088 .00052965 00000-0 17864-2 0 9996
2 65908 53.1626 83.3547 0000890 94.5638 265.5465 15.30223738 10621Epoch: 2025-12-06T16:11Z
TLE epoch observation values (Epoch: 2025-12-06T16:11:06.508Z)
Latitude
0.00005°
Longitude
124.87889°
Altitude
476.092 km
Speed
7.629 km/s
True Right ascension
05h 33m 25s
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
07:21:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.01 km
Perigee altitude
474.79 km
Semi-major axis
6,853.537 km
Eccentricity
0.00009
Inclination
53.1626°
RAAN
83.3547°
Arg. of periapsis
94.5638°
True anomaly
265.53633°
Mean anomaly
265.5465°
Eccentric anomaly
265.54142°
Mean motion
3.82535 °/min
Orbital period
94.11 mins
BSTAR
0.0017864
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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-35329 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 | 2025-12-07 09:35:40.494Z | 221.672° SW | 2025-12-07 09:38:40.494Z | 191.115° SSW | 41.34° | 2025-12-07 09:42:40.494Z | 53.796° ENE |
| 4 mins | 2025-12-07 11:15:40.494Z | 300.232° NW | 2025-12-07 11:17:40.494Z | 343.111° N | 19.104° | 2025-12-07 11:19:40.494Z | 20.174° NNE |
| 4 mins | 2025-12-07 14:33:40.494Z | 344.136° N | 2025-12-07 14:35:40.494Z | 19.004° NNE | 14.766° | 2025-12-07 14:37:40.494Z | 53.392° ENE |
| 6 mins | 2025-12-07 16:11:40.494Z | 320.634° NNW | 2025-12-07 16:13:40.494Z | 359.386° N | 38.847° | 2025-12-07 16:17:40.494Z | 118.024° SE |
| 5 mins | 2025-12-08 09:07:40.494Z | 208.218° SW | 2025-12-08 09:09:40.494Z | 121.134° SE | 40.78° | 2025-12-08 09:12:40.494Z | 57.646° ENE |
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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