STARLINK-11565, 62912
Orbit data source: Space-Track
STARLINK-11565, 62912 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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62912 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: 10 hours ago
TLE from 10 hours ago
0 STARLINK-11565
1 62912U 25027F 26032.49128860 .00338270 00000-0 25178-2 0 9995
2 62912 42.9994 205.4458 0002894 277.2805 82.7733 15.70991745 57461Epoch: 2026-02-01T11:47Z
TLE epoch observation values (Epoch: 2026-02-01T11:47:27.335Z)
Latitude
-0.00005°
Longitude
-103.11831°
Altitude
355.588 km
Speed
7.698 km/s
True Right ascension
13h 41m 46s
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
23:44:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.993 km
Perigee altitude
356.094 km
Semi-major axis
6,736.18 km
Eccentricity
0.00029
Inclination
42.9994°
RAAN
205.4458°
Arg. of periapsis
277.2805°
True anomaly
82.8062°
Mean anomaly
82.7733°
Eccentric anomaly
82.78975°
Mean motion
3.92575 °/min
Orbital period
91.7 mins
BSTAR
0.0025178
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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-11565 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 | 2026-02-02 15:31:09.063Z | 247.478° WSW | 2026-02-02 15:32:09.063Z | 239.988° WSW | 41.989° | 2026-02-02 15:35:09.063Z | 72.609° E |
| 4 mins | 2026-02-02 17:07:09.063Z | 295.26° NW | 2026-02-02 17:09:09.063Z | 25.121° NE | 32.594° | 2026-02-02 17:11:09.063Z | 69.47° E |
| 4 mins | 2026-02-02 18:43:09.063Z | 293.764° NW | 2026-02-02 18:45:09.063Z | 46.767° ENE | 42.664° | 2026-02-02 18:47:09.063Z | 98.076° 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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