STARLINK-11569, 62910
Orbit data source: Space-Track
STARLINK-11569, 62910 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 08 Feb 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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62910 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: 1 day ago
TLE from 1 day ago
0 STARLINK-11569
1 62910U 25027D 26133.22826492 .00222905 00000-0 16867-2 0 9994
2 62910 42.9991 318.5346 0001839 280.5059 79.5602 15.70949012 73304Epoch: 2026-05-13T05:28Z
TLE epoch observation values (Epoch: 2026-05-13T05:28:42.089Z)
Latitude
0.00004°
Longitude
5.36797°
Altitude
355.73 km
Speed
7.698 km/s
True Right ascension
21h 14m 08s
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
15:26:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.404 km
Perigee altitude
356.927 km
Semi-major axis
6,736.302 km
Eccentricity
0.00018
Inclination
42.9991°
RAAN
318.5346°
Arg. of periapsis
280.5059°
True anomaly
79.58093°
Mean anomaly
79.5602°
Eccentric anomaly
79.57056°
Mean motion
3.92564 °/min
Orbital period
91.7 mins
BSTAR
0.0016867
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Other satellites on launch #27 in the year 2025 (2025-02-08 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-11569 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 | 2026-05-14 15:15:28.616Z | 202.725° SW | 2026-05-14 15:17:28.616Z | 139.945° SSE | 25.324° | 2026-05-14 15:19:28.616Z | 91.568° ESE |
| 4 mins | 2026-05-14 16:51:28.616Z | 269.676° W | 2026-05-14 16:53:28.616Z | 24.889° NE | 40.004° | 2026-05-14 16:55:28.616Z | 67.091° ENE |
| 4 mins | 2026-05-14 20:04:28.616Z | 279.111° WNW | 2026-05-14 20:05:28.616Z | 229.926° WSW | 43.481° | 2026-05-14 20:08:28.616Z | 116.029° 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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