STARLINK-35272, 65899
Orbit data source: Space-Track
STARLINK-35272, 65899 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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65899 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-35272
1 65899U 25224T 26062.12900094 .00031134 00000-0 10594-2 0 9996
2 65899 53.1624 41.5418 0001567 86.7334 273.3846 15.30184758 23867Epoch: 2026-03-03T03:05Z
TLE epoch observation values (Epoch: 2026-03-03T03:05:45.681Z)
Latitude
-0.00001°
Longitude
-165.81104°
Altitude
476.097 km
Speed
7.629 km/s
True Right ascension
02h 46m 10s
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
17:47:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.591 km
Perigee altitude
474.443 km
Semi-major axis
6,853.654 km
Eccentricity
0.00016
Inclination
53.1624°
RAAN
41.5418°
Arg. of periapsis
86.7334°
True anomaly
273.36667°
Mean anomaly
273.3846°
Eccentric anomaly
273.37564°
Mean motion
3.82525 °/min
Orbital period
94.11 mins
BSTAR
0.0010594
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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-35272 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 | 2026-03-04 01:13:13.413Z | 228.51° WSW | 2026-03-04 01:16:13.413Z | 219.746° SW | 44.819° | 2026-03-04 01:19:13.413Z | 50.25° ENE |
| 4 mins | 2026-03-04 02:53:13.413Z | 308.233° NW | 2026-03-04 02:54:13.413Z | 327.82° NNW | 17.247° | 2026-03-04 02:57:13.413Z | 22.862° NE |
| 5 mins | 2026-03-04 07:49:13.413Z | 316.704° NNW | 2026-03-04 07:51:13.413Z | 10.557° NNE | 43.495° | 2026-03-04 07:54:13.413Z | 123.073° SE |
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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