STARLINK-32632, 62262
Orbit data source: Space-Track
STARLINK-32632, 62262 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 05 Dec 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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62262 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: 12 hours ago
TLE from 12 hours ago
0 STARLINK-32632
1 62262U 24231V 25352.08988404 .00007262 00000-0 25704-3 0 9996
2 62262 53.1600 238.7529 0000930 77.2912 282.8192 15.30203253 59270Epoch: 2025-12-18T02:09Z
TLE epoch observation values (Epoch: 2025-12-18T02:09:25.981Z)
Latitude
-0.00005°
Longitude
119.44422°
Altitude
475.964 km
Speed
7.629 km/s
True Right ascension
15h 55m 00s
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
12:55:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.099 km
Perigee altitude
474.824 km
Semi-major axis
6,853.599 km
Eccentricity
0.00009
Inclination
53.16°
RAAN
238.7529°
Arg. of periapsis
77.2912°
True anomaly
282.80881°
Mean anomaly
282.8192°
Eccentric anomaly
282.814°
Mean motion
3.8253 °/min
Orbital period
94.11 mins
BSTAR
0.00025704
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Other satellites on launch #231 in the year 2024 (2024-12-05 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-32632 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 | 2025-12-18 19:36:43.286Z | 244.65° WSW | 2025-12-18 19:38:43.286Z | 4.122° NNE | 41.841° | 2025-12-18 19:41:43.286Z | 45.581° ENE |
| 5 mins | 2025-12-19 00:32:43.286Z | 339.01° N | 2025-12-19 00:34:43.286Z | 14.007° NNE | 17.748° | 2025-12-19 00:37:43.286Z | 69.189° E |
| 5 mins | 2025-12-19 02:11:43.286Z | 307.33° NW | 2025-12-19 02:13:43.286Z | 149.907° SSE | 43.794° | 2025-12-19 02:16:43.286Z | 133.314° 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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