STARLINK-11510, 62516
Orbit data source: Space-Track
STARLINK-11510, 62516 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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62516 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: 1 day ago
TLE from 1 day ago
0 STARLINK-11510
1 62516U 25004F 26036.94994532 .00104227 00000-0 80483-3 0 9995
2 62516 42.9990 262.3184 0002105 259.6508 100.4123 15.70862202 62219Epoch: 2026-02-05T22:47Z
TLE epoch observation values (Epoch: 2026-02-05T22:47:55.275Z)
Latitude
0.00002°
Longitude
144.24328°
Altitude
356.459 km
Speed
7.697 km/s
True Right ascension
17h 29m 16s
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
11:31:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.831 km
Perigee altitude
356.995 km
Semi-major axis
6,736.55 km
Eccentricity
0.00021
Inclination
42.999°
RAAN
262.3184°
Arg. of periapsis
259.6508°
True anomaly
100.43602°
Mean anomaly
100.4123°
Eccentric anomaly
100.42416°
Mean motion
3.92543 °/min
Orbital period
91.71 mins
BSTAR
0.00080483
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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-11510 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 | 2026-02-07 17:44:29.437Z | 205.518° SW | 2026-02-07 17:46:29.437Z | 138.48° SSE | 27.043° | 2026-02-07 17:48:29.437Z | 89.804° E |
| 4 mins | 2026-02-07 19:20:29.437Z | 272.138° WNW | 2026-02-07 19:22:29.437Z | 20.492° NNE | 39.483° | 2026-02-07 19:24:29.437Z | 66.549° ENE |
| 4 mins | 2026-02-07 22:33:29.437Z | 276.368° WNW | 2026-02-07 22:34:29.437Z | 231.629° WSW | 42.179° | 2026-02-07 22:37:29.437Z | 118.735° 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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