STARLINK-11482, 62520
Orbit data source: Space-Track
STARLINK-11482, 62520 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 08 Jan 2025 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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62520 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 V2MD, Unknown motor
Mass
960 kg wet, ~910 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 18.1 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 STARLINK-11482
1 62520U 25004K 26008.86730175 .00188631 00000-0 14377-2 0 9990
2 62520 42.9993 70.9921 0000812 358.3791 1.7074 15.70884388 57809Epoch: 2026-01-08T20:48Z
TLE epoch observation values (Epoch: 2026-01-08T20:48:54.871Z)
Latitude
0°
Longitude
10.34823°
Altitude
355.593 km
Speed
7.698 km/s
True Right ascension
04h 43m 58s
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
13:20:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
358.897 km
Perigee altitude
357.803 km
Semi-major axis
6,736.487 km
Eccentricity
0.00008
Inclination
42.9993°
RAAN
70.9921°
Arg. of periapsis
358.3791°
True anomaly
1.70768°
Mean anomaly
1.7074°
Eccentric anomaly
1.70754°
Mean motion
3.92548 °/min
Orbital period
91.71 mins
BSTAR
0.0014377
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Other satellites on launch #4 in the year 2025 (2025-01-08 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-11482 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-01-10 06:34:37.560Z | 195.575° SSW | 2026-01-10 06:36:37.560Z | 150.121° SSE | 18.937° | 2026-01-10 06:38:37.560Z | 101.804° ESE |
| 4 mins | 2026-01-10 08:10:37.560Z | 256.675° W | 2026-01-10 08:12:37.560Z | 14.333° NNE | 44.437° | 2026-01-10 08:14:37.560Z | 69.553° E |
| 4 mins | 2026-01-10 11:23:37.560Z | 291.296° WNW | 2026-01-10 11:24:37.560Z | 301.154° NW | 41.507° | 2026-01-10 11:27:37.560Z | 105.757° 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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