STARLINK-11516, 62522
Orbit data source: Space-Track
STARLINK-11516, 62522 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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62522 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: 17 hours ago
TLE from 17 hours ago
0 STARLINK-11516
1 62522U 25004M 26094.91125507 .00140938 00000-0 10813-2 0 9999
2 62522 43.0018 272.5679 0002646 264.9478 95.1087 15.70882948 71337Epoch: 2026-04-04T21:52Z
TLE epoch observation values (Epoch: 2026-04-04T21:52:12.438Z)
Latitude
-0.00005°
Longitude
111.29179°
Altitude
356.303 km
Speed
7.697 km/s
True Right ascension
18h 10m 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
21:14:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
360.136 km
Perigee altitude
356.571 km
Semi-major axis
6,736.491 km
Eccentricity
0.00026
Inclination
43.0018°
RAAN
272.5679°
Arg. of periapsis
264.9478°
True anomaly
95.1389°
Mean anomaly
95.1087°
Eccentric anomaly
95.1238°
Mean motion
3.92548 °/min
Orbital period
91.71 mins
BSTAR
0.0010813
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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-11516 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 | 2026-04-05 16:27:33.298Z | 262.431° W | 2026-04-05 16:29:33.298Z | 356.212° N | 43.335° | 2026-04-05 16:31:33.298Z | 67.403° ENE |
| 4 mins | 2026-04-05 18:04:33.298Z | 305.703° NW | 2026-04-05 18:05:33.298Z | 345.993° N | 33.879° | 2026-04-05 18:08:33.298Z | 75.951° E |
| 4 mins | 2026-04-05 19:40:33.298Z | 286.735° WNW | 2026-04-05 19:41:33.298Z | 282.163° WNW | 40.606° | 2026-04-05 19:44:33.298Z | 110.964° 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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