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, 14.5 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 STARLINK-11482
1 62520U 25004K 25256.17486636 .00297600 00000-0 22332-2 0 9995
2 62520 43.0007 60.4076 0000868 332.7883 27.2939 15.70919223 39294Epoch: 2025-09-13T04:11Z
TLE epoch observation values (Epoch: 2025-09-13T04:11:48.453Z)
Latitude
-0.00003°
Longitude
5.04368°
Altitude
355.52 km
Speed
7.698 km/s
True Right ascension
04h 01m 37s
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
08:49:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
358.835 km
Perigee altitude
357.665 km
Semi-major axis
6,736.387 km
Eccentricity
0.00009
Inclination
43.0007°
RAAN
60.4076°
Arg. of periapsis
332.7883°
True anomaly
27.29846°
Mean anomaly
27.2939°
Eccentric anomaly
27.29618°
Mean motion
3.92557 °/min
Orbital period
91.71 mins
BSTAR
0.0022332
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-13 16:43:14.591Z | 282.708° WNW | 2025-09-13 16:45:14.591Z | 338.494° N | 35.132° | 2025-09-13 16:48:14.591Z | 69.551° E |
| 4 mins | 2025-09-13 18:20:14.591Z | 299.954° NW | 2025-09-13 18:22:14.591Z | 54.41° ENE | 36.852° | 2025-09-13 18:24:14.591Z | 90.526° ESE |
| 4 mins | 2025-09-13 19:56:14.591Z | 261.821° W | 2025-09-13 19:58:14.591Z | 185.211° SSW | 27.881° | 2025-09-13 20:00:14.591Z | 142.394° SSE |
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
Authenticating...
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