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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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: 16 hours ago
TLE from 16 hours ago
0 STARLINK-11516
1 62522U 25004M 25308.51972962 .00370732 00000-0 27393-2 0 9995
2 62522 42.9994 105.1113 0003142 254.1719 105.8802 15.71069045 47527Epoch: 2025-11-04T12:28Z
TLE epoch observation values (Epoch: 2025-11-04T12:28:24.639Z)
Latitude
-0.00003°
Longitude
-125.99698°
Altitude
356.191 km
Speed
7.697 km/s
True Right ascension
07h 00m 26s
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
00:23:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.939 km
Perigee altitude
355.706 km
Semi-major axis
6,735.959 km
Eccentricity
0.00031
Inclination
42.9994°
RAAN
105.1113°
Arg. of periapsis
254.1719°
True anomaly
105.91483°
Mean anomaly
105.8802°
Eccentric anomaly
105.89751°
Mean motion
3.92594 °/min
Orbital period
91.7 mins
BSTAR
0.0027393
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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 | 2025-11-05 14:40:39.957Z | 244.847° WSW | 2025-11-05 14:41:39.957Z | 208.209° SW | 44.482° | 2025-11-05 14:44:39.957Z | 72.811° E |
| 4 mins | 2025-11-05 16:16:39.957Z | 299.68° NW | 2025-11-05 16:17:39.957Z | 337.745° N | 33.6° | 2025-11-05 16:20:39.957Z | 71.079° E |
| 4 mins | 2025-11-05 17:52:39.957Z | 295.965° NW | 2025-11-05 17:54:39.957Z | 70.586° E | 39.353° | 2025-11-05 17:56:39.957Z | 98.064° 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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