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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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: 14 hours ago
TLE from 14 hours ago
0 STARLINK-11482
1 62520U 25004K 26305.75003472 .00232102 00000-0 17149-2 0 9994
2 62520 43.0006 81.4767 0001430 278.2955 155.0422 15.71488407 5918Epoch: 2026-11-01T18:00Z
TLE epoch observation values (Epoch: 2026-11-01T18:00:02.999Z)
Latitude
40.95295°
Longitude
-161.84307°
Altitude
358.155 km
Speed
7.7 km/s
True Right ascension
09h 56m 49s
True Declination
40° 46' 22"
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
04:14:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
357.588 km
Perigee altitude
355.661 km
Semi-major axis
6,734.761 km
Eccentricity
0.00014
Inclination
43.0006°
RAAN
81.4767°
Arg. of periapsis
278.2955°
True anomaly
155.04911°
Mean anomaly
155.0422°
Eccentric anomaly
155.04566°
Mean motion
3.92699 °/min
Orbital period
91.67 mins
BSTAR
0.0017149
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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 | 2026-11-02 12:11:52.942Z | 196.812° SSW | 2026-11-02 12:13:52.942Z | 143.804° SSE | 23.26° | 2026-11-02 12:15:52.942Z | 96.368° ESE |
| 4 mins | 2026-11-02 13:47:52.942Z | 262.581° W | 2026-11-02 13:49:52.942Z | 31.809° NE | 64.26° | 2026-11-02 13:51:52.942Z | 68.081° E |
| 4 mins | 2026-11-02 17:00:52.942Z | 289.083° WNW | 2026-11-02 17:01:52.942Z | 292.5° NW | 78.743° | 2026-11-02 17:04:52.942Z | 108.986° 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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