STARLINK-35278, 65902
Orbit data source: Space-Track
STARLINK-35278, 65902 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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65902 intel report (Beta)
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Edit Public Description
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: 23 hours ago
TLE from 23 hours ago
0 STARLINK-35278
1 65902U 25224W 26022.92336891 .00045898 00000-0 15518-2 0 9996
2 65902 53.1559 224.1781 0001379 123.9049 236.2083 15.30207964 17868Epoch: 2026-01-22T22:09Z
TLE epoch observation values (Epoch: 2026-01-22T22:09:39.073Z)
Latitude
-0.00004°
Longitude
129.4957°
Altitude
476.616 km
Speed
7.628 km/s
True Right ascension
14h 56m 42s
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
22:16:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.393 km
Perigee altitude
474.503 km
Semi-major axis
6,853.585 km
Eccentricity
0.00014
Inclination
53.1559°
RAAN
224.1781°
Arg. of periapsis
123.9049°
True anomaly
236.19517°
Mean anomaly
236.2083°
Eccentric anomaly
236.20173°
Mean motion
3.82531 °/min
Orbital period
94.11 mins
BSTAR
0.0015518
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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-35278 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-01-23 22:08:33.161Z | 322.112° NNW | 2026-01-23 22:11:33.161Z | 16.026° NNE | 32.664° | 2026-01-23 22:14:33.161Z | 100.339° ESE |
| 4 mins | 2026-01-23 23:48:33.161Z | 257.08° W | 2026-01-23 23:49:33.161Z | 232.67° WSW | 21.511° | 2026-01-23 23:52:33.161Z | 176.54° S |
| 5 mins | 2026-01-24 15:05:33.161Z | 189.046° SSW | 2026-01-24 15:07:33.161Z | 127.611° SE | 31.894° | 2026-01-24 15:10:33.161Z | 65.904° ENE |
| 5 mins | 2026-01-24 16:43:33.161Z | 284.663° WNW | 2026-01-24 16:45:33.161Z | 336.182° NNW | 25.465° | 2026-01-24 16:48:33.161Z | 31.974° NE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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