STARLINK-32492, 62050
Orbit data source: Space-Track
STARLINK-32492, 62050 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 21 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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62050 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, 17.7 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-32492
1 62050U 24216U 25311.79897798 .00058482 00000-0 21170-2 0 9994
2 62050 42.9991 231.6514 0001623 271.0409 89.0257 15.27594441 55155Epoch: 2025-11-07T19:10Z
TLE epoch observation values (Epoch: 2025-11-07T19:10:31.697Z)
Latitude
0°
Longitude
-103.21843°
Altitude
482.762 km
Speed
7.626 km/s
True Right ascension
15h 26m 36s
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
03:44:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.065 km
Perigee altitude
483.837 km
Semi-major axis
6,863.088 km
Eccentricity
0.00016
Inclination
42.9991°
RAAN
231.6514°
Arg. of periapsis
271.0409°
True anomaly
89.0443°
Mean anomaly
89.0257°
Eccentric anomaly
89.035°
Mean motion
3.81737 °/min
Orbital period
94.31 mins
BSTAR
0.002117
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Other satellites on launch #216 in the year 2024 (2024-11-21 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-32492 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 | 2025-11-09 21:36:19.353Z | 218.032° SW | 2025-11-09 21:39:19.353Z | 131.627° SE | 33.232° | 2025-11-09 21:42:19.353Z | 80.713° E |
| 6 mins | 2025-11-09 23:15:19.353Z | 271.144° WNW | 2025-11-09 23:17:19.353Z | 309.754° NW | 39.85° | 2025-11-09 23:21:19.353Z | 70.618° E |
| 6 mins | 2025-11-10 00:54:19.353Z | 292.088° WNW | 2025-11-10 00:57:19.353Z | 31.759° NE | 38.492° | 2025-11-10 01:00:19.353Z | 84.983° E |
| 6 mins | 2025-11-10 02:33:19.353Z | 280.894° WNW | 2025-11-10 02:36:19.353Z | 174° S | 40.04° | 2025-11-10 02:39:19.353Z | 124.713° 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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