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: 15 hours ago
TLE from 15 hours ago
0 STARLINK-11516
1 62522U 25004M 26305.74621431 .00179412 00000-0 13260-2 0 9990
2 62522 43.0007 81.6257 0001897 260.4030 99.6623 15.71645565104490Epoch: 2026-11-01T17:54Z
TLE epoch observation values (Epoch: 2026-11-01T17:54:32.916Z)
Latitude
-0.00006°
Longitude
131.95532°
Altitude
354.179 km
Speed
7.698 km/s
True Right ascension
05h 26m 30s
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
04:14:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
357.453 km
Perigee altitude
354.898 km
Semi-major axis
6,734.313 km
Eccentricity
0.00019
Inclination
43.0007°
RAAN
81.6257°
Arg. of periapsis
260.403°
True anomaly
99.68373°
Mean anomaly
99.6623°
Eccentric anomaly
99.67301°
Mean motion
3.92738 °/min
Orbital period
91.66 mins
BSTAR
0.001326
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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 | 2026-11-02 12:25:37.321Z | 202.868° SW | 2026-11-02 12:27:37.321Z | 138.848° SSE | 28.852° | 2026-11-02 12:29:37.321Z | 90.891° ESE |
| 4 mins | 2026-11-02 14:01:37.321Z | 270.794° WNW | 2026-11-02 14:03:37.321Z | 26.373° NE | 55.203° | 2026-11-02 14:05:37.321Z | 66.685° ENE |
| 4 mins | 2026-11-02 17:14:37.321Z | 279.563° WNW | 2026-11-02 17:15:37.321Z | 217.529° SW | 74.698° | 2026-11-02 17:18:37.321Z | 115.508° 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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