STARLINK-32808, 62863
Orbit data source: Space-Track
STARLINK-32808, 62863 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 01 Feb 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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62863 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: 8 hours ago
TLE from 8 hours ago
0 STARLINK-32808
1 62863U 25022K 25259.27257933 .00027006 00000-0 91965-3 0 9995
2 62863 53.1575 219.9361 0000935 98.6776 261.4331 15.30234539 35197Epoch: 2025-09-16T06:32Z
TLE epoch observation values (Epoch: 2025-09-16T06:32:30.854Z)
Latitude
0.00002°
Longitude
126.3423°
Altitude
476.107 km
Speed
7.629 km/s
True Right ascension
14h 39m 44s
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
07:38:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.01 km
Perigee altitude
474.728 km
Semi-major axis
6,853.506 km
Eccentricity
0.00009
Inclination
53.1575°
RAAN
219.9361°
Arg. of periapsis
98.6776°
True anomaly
261.42251°
Mean anomaly
261.4331°
Eccentric anomaly
261.4278°
Mean motion
3.82537 °/min
Orbital period
94.11 mins
BSTAR
0.00091965
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Other satellites on launch #22 in the year 2025 (2025-02-01 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-32808 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 | 2025-09-16 23:56:58.164Z | 217.105° SW | 2025-09-16 23:59:58.164Z | 169.566° S | 40.397° | 2025-09-17 00:02:58.164Z | 58.85° ENE |
| 4 mins | 2025-09-17 01:36:58.164Z | 300.359° NW | 2025-09-17 01:38:58.164Z | 346.404° N | 20.043° | 2025-09-17 01:40:58.164Z | 22.608° NE |
| 5 mins | 2025-09-17 06:32:58.164Z | 324.295° NNW | 2025-09-17 06:34:58.164Z | 11.998° NNE | 37.599° | 2025-09-17 06:37:58.164Z | 109.951° ESE |
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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