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: 3 days ago
TLE from 3 days ago
0 STARLINK-11516
1 62522U 25004M 26252.40675125 .00146650 00000-0 11232-2 0 9998
2 62522 43.0007 43.2316 0002440 234.1130 125.9511 15.70905526 96106Epoch: 2026-09-09T09:45Z
TLE epoch observation values (Epoch: 2026-09-09T09:45:43.307Z)
Latitude
-0.00006°
Longitude
-91.65818°
Altitude
357.044 km
Speed
7.696 km/s
True Right ascension
02h 52m 55s
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
21:33:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.933 km
Perigee altitude
356.646 km
Semi-major axis
6,736.426 km
Eccentricity
0.00024
Inclination
43.0007°
RAAN
43.2316°
Arg. of periapsis
234.113°
True anomaly
125.97373°
Mean anomaly
125.9511°
Eccentric anomaly
125.96242°
Mean motion
3.92553 °/min
Orbital period
91.71 mins
BSTAR
0.0011232
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-12 12:44:04.603Z | 229.564° WSW | 2026-09-12 12:47:04.603Z | 121.217° SE | 43.553° | 2026-09-12 12:49:04.603Z | 80.844° E |
| 4 mins | 2026-09-12 14:21:04.603Z | 284.674° WNW | 2026-09-12 14:23:04.603Z | 21.313° NNE | 44.743° | 2026-09-12 14:25:04.603Z | 65.898° ENE |
| 4 mins | 2026-09-12 15:57:04.603Z | 298.117° NW | 2026-09-12 15:59:04.603Z | 18.08° NNE | 49.749° | 2026-09-12 16:01:04.603Z | 81.951° E |
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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