STARLINK-32920, 62925
Orbit data source: Space-Track
STARLINK-32920, 62925 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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62925 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: 2 days ago
TLE from 2 days ago
0 STARLINK-32920
1 62925U 25027U 25259.83223905 .00028780 00000-0 10510-2 0 9999
2 62925 43.0034 30.6674 0001955 265.5255 94.5373 15.27589878 34958Epoch: 2025-09-16T19:58Z
TLE epoch observation values (Epoch: 2025-09-16T19:58:25.453Z)
Latitude
-0.00006°
Longitude
95.04439°
Altitude
482.902 km
Speed
7.626 km/s
True Right ascension
02h 02m 40s
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
09:05:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.306 km
Perigee altitude
483.622 km
Semi-major axis
6,863.101 km
Eccentricity
0.0002
Inclination
43.0034°
RAAN
30.6674°
Arg. of periapsis
265.5255°
True anomaly
94.55963°
Mean anomaly
94.5373°
Eccentric anomaly
94.54847°
Mean motion
3.81736 °/min
Orbital period
94.31 mins
BSTAR
0.001051
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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-32920 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-18 16:20:05.377Z | 287.376° WNW | 2025-09-18 16:24:05.377Z | 135.446° SSE | 43.959° | 2025-09-18 16:27:05.377Z | 112.726° SE |
| 4 mins | 2025-09-18 18:01:05.377Z | 243.446° WSW | 2025-09-18 18:02:05.377Z | 222.747° SW | 18.802° | 2025-09-18 18:05:05.377Z | 168.128° S |
| 5 mins | 2025-09-19 10:57:05.377Z | 193.253° SSW | 2025-09-19 10:59:05.377Z | 142.839° SSE | 25.624° | 2025-09-19 11:02:05.377Z | 87.893° E |
| 6 mins | 2025-09-19 12:35:05.377Z | 258.962° W | 2025-09-19 12:38:05.377Z | 44.983° NE | 42.377° | 2025-09-19 12:41:05.377Z | 70.73° E |
| 5 mins | 2025-09-19 14:15:05.377Z | 297.89° NW | 2025-09-19 14:17:05.377Z | 19.009° NNE | 37.6° | 2025-09-19 14:20:05.377Z | 78.019° E |
| 5 mins | 2025-09-19 15:54:05.377Z | 286.305° WNW | 2025-09-19 15:56:05.377Z | 142.343° SSE | 44.613° | 2025-09-19 15:59:05.377Z | 111.925° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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