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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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: 17 hours ago
TLE from 17 hours ago
0 STARLINK-32632
1 62262U 24231V 26316.90432884 .00017709 00000-0 58070-3 0 9993
2 62262 53.1572 145.1045 0001087 106.8555 253.2566 15.31720367109799Epoch: 2026-11-12T21:42Z
TLE epoch observation values (Epoch: 2026-11-12T21:42:14.011Z)
Latitude
-0.00001°
Longitude
127.51498°
Altitude
471.794 km
Speed
7.631 km/s
True Right ascension
09h 40m 25s
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
11:07:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.681 km
Perigee altitude
470.192 km
Semi-major axis
6,849.073 km
Eccentricity
0.00011
Inclination
53.1572°
RAAN
145.1045°
Arg. of periapsis
106.8555°
True anomaly
253.24467°
Mean anomaly
253.2566°
Eccentric anomaly
253.25064°
Mean motion
3.82909 °/min
Orbital period
94.02 mins
BSTAR
0.0005807
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-11-13 15:06:03.078Z | 210.583° SW | 2026-11-13 15:09:03.078Z | 117.108° SE | 53.576° | 2026-11-13 15:12:03.078Z | 58.941° ENE |
| 4 mins | 2026-11-13 16:45:03.078Z | 293.664° NW | 2026-11-13 16:47:03.078Z | 339.53° N | 23.25° | 2026-11-13 16:49:03.078Z | 19.849° NNE |
| 5 mins | 2026-11-13 21:41:03.078Z | 327.466° NNW | 2026-11-13 21:43:03.078Z | 15.329° NNE | 44.503° | 2026-11-13 21:46:03.078Z | 104.919° 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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