STARLINK-32391, 61855
Orbit data source: Space-Track
STARLINK-32391, 61855 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 07 Nov 2024 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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61855 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-32391
1 61855U 24202L 25255.47237171 -.00002483 00000-0 -80793-4 0 9996
2 61855 43.0029 164.2928 0001000 271.2434 88.8304 15.27559713 48076Epoch: 2025-09-12T11:20Z
TLE epoch observation values (Epoch: 2025-09-12T11:20:12.915Z)
Latitude
0.00003°
Longitude
2.51943°
Altitude
482.872 km
Speed
7.626 km/s
True Right ascension
10h 57m 10s
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
13:04:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.741 km
Perigee altitude
484.368 km
Semi-major axis
6,863.192 km
Eccentricity
0.0001
Inclination
43.0029°
RAAN
164.2928°
Arg. of periapsis
271.2434°
True anomaly
88.84186°
Mean anomaly
88.8304°
Eccentric anomaly
88.83613°
Mean motion
3.81728 °/min
Orbital period
94.31 mins
BSTAR
-0.000080793
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Other satellites on launch #202 in the year 2024 (2024-11-07 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-32391 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 | 2025-09-13 22:07:52.228Z | 253.186° W | 2025-09-13 22:09:52.228Z | 264.342° W | 44.049° | 2025-09-13 22:13:52.228Z | 71.708° E |
| 6 mins | 2025-09-13 23:46:52.228Z | 288.864° WNW | 2025-09-13 23:48:52.228Z | 333.204° NNW | 36.643° | 2025-09-13 23:52:52.228Z | 76.973° E |
| 6 mins | 2025-09-14 01:25:52.228Z | 289.278° WNW | 2025-09-14 01:28:52.228Z | 94.497° ESE | 43.044° | 2025-09-14 01:31:52.228Z | 106.573° ESE |
| 4 mins | 2025-09-14 03:05:52.228Z | 244.915° WSW | 2025-09-14 03:06:52.228Z | 221.002° SW | 22.596° | 2025-09-14 03:09:52.228Z | 160.89° S |
| 4 mins | 2025-09-14 20:01:52.228Z | 187.003° SSW | 2025-09-14 20:03:52.228Z | 143.585° SSE | 21.656° | 2025-09-14 20:05:52.228Z | 102.325° 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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