STARLINK-32864, 62862
Orbit data source: Space-Track
STARLINK-32864, 62862 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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62862 intel report (Beta)
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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, 17.7 m
Radar Cross Section
33.884 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 STARLINK-32864
1 62862U 25022J 26306.43349887 .00015533 00000-0 47020-3 0 9991
2 62862 53.1572 100.7793 0001650 78.4863 281.6325 15.34379813 98361Epoch: 2026-11-02T10:24Z
TLE epoch observation values (Epoch: 2026-11-02T10:24:14.302Z)
Latitude
0°
Longitude
-96.99087°
Altitude
463.437 km
Speed
7.636 km/s
True Right ascension
06h 43m 07s
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
00:23:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.149 km
Perigee altitude
461.892 km
Semi-major axis
6,841.158 km
Eccentricity
0.00017
Inclination
53.1572°
RAAN
100.7793°
Arg. of periapsis
78.4863°
True anomaly
281.61398°
Mean anomaly
281.6325°
Eccentric anomaly
281.62324°
Mean motion
3.83574 °/min
Orbital period
93.85 mins
BSTAR
0.0004702
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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-32864 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-11-03 13:10:57.380Z | 237.212° WSW | 2026-11-03 13:12:57.380Z | 348.295° N | 76.178° | 2026-11-03 13:15:57.380Z | 46.957° ENE |
| 4 mins | 2026-11-03 18:06:57.380Z | 348.045° N | 2026-11-03 18:08:57.380Z | 26.877° NE | 17.17° | 2026-11-03 18:10:57.380Z | 62.044° ENE |
| 5 mins | 2026-11-03 19:44:57.380Z | 313.802° NW | 2026-11-03 19:46:57.380Z | 88.641° E | 78.963° | 2026-11-03 19:49:57.380Z | 127.974° 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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