STARLINK-32901, 62895
Orbit data source: Space-Track
STARLINK-32901, 62895 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 04 Feb 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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62895 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 V2M, Unknown motor
Mass
730 kg wet, ~700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 14.5 m
Radar Cross Section
33.884 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 STARLINK-32901
1 62895U 25024S 25260.32700485 -.00009236 00000-0 -32653-3 0 9991
2 62895 42.9983 224.3062 0002287 248.4078 111.6530 15.27574064 35756Epoch: 2025-09-17T07:50Z
TLE epoch observation values (Epoch: 2025-09-17T07:50:53.219Z)
Latitude
-0°
Longitude
110.0799°
Altitude
483.421 km
Speed
7.625 km/s
True Right ascension
14h 57m 13s
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
01:22:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.582 km
Perigee altitude
483.443 km
Semi-major axis
6,863.149 km
Eccentricity
0.00023
Inclination
42.9983°
RAAN
224.3062°
Arg. of periapsis
248.4078°
True anomaly
111.67736°
Mean anomaly
111.653°
Eccentric anomaly
111.66518°
Mean motion
3.81731 °/min
Orbital period
94.31 mins
BSTAR
-0.00032653
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Other satellites on launch #24 in the year 2025 (2025-02-04 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-32901 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 | 2025-09-19 00:52:41.415Z | 224.717° SW | 2025-09-19 00:54:41.415Z | 183.562° SSW | 36.343° | 2025-09-19 00:58:41.415Z | 78.094° E |
| 6 mins | 2025-09-19 02:31:41.415Z | 275.721° WNW | 2025-09-19 02:33:41.415Z | 316.912° NNW | 38.797° | 2025-09-19 02:37:41.415Z | 71.129° E |
| 6 mins | 2025-09-19 04:10:41.415Z | 292.436° WNW | 2025-09-19 04:13:41.415Z | 35.046° NE | 39.639° | 2025-09-19 04:16:41.415Z | 88.5° E |
| 5 mins | 2025-09-19 05:50:41.415Z | 267.923° W | 2025-09-19 05:52:41.415Z | 183.468° SSW | 36.954° | 2025-09-19 05:55:41.415Z | 130.865° 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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