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: 10 hours ago
TLE from 10 hours ago
0 STARLINK-11482
1 62520U 25004K 26254.74340293 .00110265 00000-0 85083-3 0 9999
2 62520 43.0003 28.9257 0001949 276.0456 84.0190 15.70857117 96473Epoch: 2026-09-11T17:50Z
TLE epoch observation values (Epoch: 2026-09-11T17:50:30.013Z)
Latitude
0.00003°
Longitude
130.5383°
Altitude
356.081 km
Speed
7.697 km/s
True Right ascension
01h 55m 42s
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
20:05:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.741 km
Perigee altitude
357.115 km
Semi-major axis
6,736.565 km
Eccentricity
0.00019
Inclination
43.0003°
RAAN
28.9257°
Arg. of periapsis
276.0456°
True anomaly
84.04121°
Mean anomaly
84.019°
Eccentric anomaly
84.03011°
Mean motion
3.92541 °/min
Orbital period
91.71 mins
BSTAR
0.00085083
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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 | 2026-09-12 12:22:25.937Z | 207.434° SW | 2026-09-12 12:24:25.937Z | 139.101° SSE | 32.495° | 2026-09-12 12:26:25.937Z | 89.107° E |
| 4 mins | 2026-09-12 13:58:25.937Z | 273.274° WNW | 2026-09-12 14:00:25.937Z | 14.201° NNE | 55.301° | 2026-09-12 14:02:25.937Z | 65.577° ENE |
| 4 mins | 2026-09-12 17:11:25.937Z | 277.261° WNW | 2026-09-12 17:12:25.937Z | 241.265° WSW | 62.06° | 2026-09-12 17:15:25.937Z | 119.379° 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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