STARLINK-32508, 62158
Orbit data source: Space-Track
STARLINK-32508, 62158 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 30 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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62158 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: 23 hours ago
TLE from 23 hours ago
0 STARLINK-32508
1 62158U 24224V 25348.84269646 .00013885 00000-0 51324-3 0 9996
2 62158 43.0012 277.2842 0001397 256.2128 103.8568 15.27573406 59502Epoch: 2025-12-14T20:13Z
TLE epoch observation values (Epoch: 2025-12-14T20:13:28.974Z)
Latitude
-0.00002°
Longitude
-109.83635°
Altitude
483.074 km
Speed
7.626 km/s
True Right ascension
18h 29m 08s
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
17:25:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.973 km
Perigee altitude
484.055 km
Semi-major axis
6,863.151 km
Eccentricity
0.00014
Inclination
43.0012°
RAAN
277.2842°
Arg. of periapsis
256.2128°
True anomaly
103.87234°
Mean anomaly
103.8568°
Eccentric anomaly
103.86457°
Mean motion
3.81731 °/min
Orbital period
94.31 mins
BSTAR
0.00051324
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Other satellites on launch #224 in the year 2024 (2024-11-30 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-32508 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 | 2025-12-15 23:08:28.832Z | 235.818° WSW | 2025-12-15 23:11:28.832Z | 120.614° SE | 41.073° | 2025-12-15 23:14:28.832Z | 75.593° E |
| 5 mins | 2025-12-16 00:48:28.832Z | 288.819° WNW | 2025-12-16 00:50:28.832Z | 16.838° NNE | 38.242° | 2025-12-16 00:53:28.832Z | 71.641° E |
| 5 mins | 2025-12-16 02:27:28.832Z | 296.732° NW | 2025-12-16 02:29:28.832Z | 25.057° NE | 42.144° | 2025-12-16 02:32:28.832Z | 93.612° ESE |
| 5 mins | 2025-12-16 04:06:28.832Z | 262.684° W | 2025-12-16 04:08:28.832Z | 197.638° SSW | 32.202° | 2025-12-16 04:11:28.832Z | 140.288° SSE |
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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