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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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: 22 hours ago
TLE from 22 hours ago
0 STARLINK-11569
1 62910U 25027D 25347.15466302 .00329830 00000-0 24515-2 0 9996
2 62910 42.9967 149.1616 0001550 332.3014 27.7771 15.71050764 49541Epoch: 2025-12-13T03:42Z
TLE epoch observation values (Epoch: 2025-12-13T03:42:42.884Z)
Latitude
-0.00003°
Longitude
11.39688°
Altitude
354.74 km
Speed
7.699 km/s
True Right ascension
09h 56m 38s
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
23:53:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
358.919 km
Perigee altitude
356.831 km
Semi-major axis
6,736.012 km
Eccentricity
0.00016
Inclination
42.9967°
RAAN
149.1616°
Arg. of periapsis
332.3014°
True anomaly
27.78538°
Mean anomaly
27.7771°
Eccentric anomaly
27.78124°
Mean motion
3.9259 °/min
Orbital period
91.7 mins
BSTAR
0.0024515
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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
Loading observer location...
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 | 2025-12-14 15:04:28.340Z | 255.103° W | 2025-12-14 15:05:28.340Z | 275.675° WNW | 44.434° | 2025-12-14 15:08:28.340Z | 71.312° E |
| 4 mins | 2025-12-14 16:40:28.340Z | 300.997° NW | 2025-12-14 16:41:28.340Z | 336.877° NNW | 32.948° | 2025-12-14 16:44:28.340Z | 72.413° E |
| 4 mins | 2025-12-14 18:16:28.340Z | 292.587° NW | 2025-12-14 18:18:28.340Z | 85.546° E | 40.683° | 2025-12-14 18:20:28.340Z | 103.104° 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
Authenticating...
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