STARLINK-32921, 62920
Orbit data source: Space-Track
STARLINK-32921, 62920 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 08 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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62920 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-32921
1 62920U 25027P 26302.18266545 .00040528 00000-0 11653-2 0 9992
2 62920 42.9983 247.4972 0007387 157.7607 202.3569 15.35106020 97285Epoch: 2026-10-29T04:23Z
TLE epoch observation values (Epoch: 2026-10-29T04:23:02.294Z)
Latitude
-0.00003°
Longitude
144.21685°
Altitude
465.052 km
Speed
7.633 km/s
True Right ascension
16h 29m 59s
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
18:23:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
467.611 km
Perigee altitude
457.504 km
Semi-major axis
6,840.694 km
Eccentricity
0.00074
Inclination
42.9983°
RAAN
247.4972°
Arg. of periapsis
157.7607°
True anomaly
202.32473°
Mean anomaly
202.3569°
Eccentric anomaly
202.34081°
Mean motion
3.83613 °/min
Orbital period
93.84 mins
BSTAR
0.0011653
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Other satellites on launch #27 in the year 2025 (2025-02-08 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-32921 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 | 2026-10-29 23:18:35.619Z | 201.931° SSW | 2026-10-29 23:21:35.619Z | 142.14° SSE | 25.098° | 2026-10-29 23:23:35.619Z | 99.419° ESE |
| 5 mins | 2026-10-30 00:57:35.619Z | 256.62° W | 2026-10-30 00:59:35.619Z | 332.275° NNW | 81.848° | 2026-10-30 01:02:35.619Z | 70.41° E |
| 5 mins | 2026-10-30 02:36:35.619Z | 297.957° NW | 2026-10-30 02:38:35.619Z | 20.622° NNE | 47.605° | 2026-10-30 02:41:35.619Z | 76.366° E |
| 5 mins | 2026-10-30 04:14:35.619Z | 289.417° WNW | 2026-10-30 04:16:35.619Z | 300.229° NW | 73.309° | 2026-10-30 04:19:35.619Z | 107.206° ESE |
| 4 mins | 2026-10-30 05:53:35.619Z | 248.318° W | 2026-10-30 05:54:35.619Z | 226.09° WSW | 22.303° | 2026-10-30 05:57:35.619Z | 163.84° S |
| 4 mins | 2026-10-30 22:44:35.619Z | 184.1° SSW | 2026-10-30 22:46:35.619Z | 139.811° SSE | 21.851° | 2026-10-30 22:48:35.619Z | 100.657° ESE |
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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