STARLINK-11566, 62914
Orbit data source: Space-Track
STARLINK-11566, 62914 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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62914 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: 11 hours ago
TLE from 11 hours ago
0 STARLINK-11566
1 62914U 25027H 25312.59198394 .00301333 00000-0 22636-2 0 9993
2 62914 42.9981 357.8669 0005159 26.5755 333.5376 15.70874965 44146Epoch: 2025-11-08T14:12Z
TLE epoch observation values (Epoch: 2025-11-08T14:12:27.412Z)
Latitude
-0.00004°
Longitude
96.73326°
Altitude
353.057 km
Speed
7.701 km/s
True Right ascension
23h 51m 28s
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
21:28:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
361.852 km
Perigee altitude
354.902 km
Semi-major axis
6,736.514 km
Eccentricity
0.00052
Inclination
42.9981°
RAAN
357.8669°
Arg. of periapsis
26.5755°
True anomaly
333.51124°
Mean anomaly
333.5376°
Eccentric anomaly
333.52442°
Mean motion
3.92546 °/min
Orbital period
91.71 mins
BSTAR
0.0022636
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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-11566 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 | 2025-11-09 08:51:19.700Z | 297.413° NW | 2025-11-09 08:52:19.700Z | 337.577° N | 34.313° | 2025-11-09 08:55:19.700Z | 69.999° E |
| 4 mins | 2025-11-09 10:27:19.700Z | 298.453° NW | 2025-11-09 10:29:19.700Z | 58.489° ENE | 38.015° | 2025-11-09 10:31:19.700Z | 93.219° ESE |
| 4 mins | 2025-11-09 12:03:19.700Z | 258.836° W | 2025-11-09 12:05:19.700Z | 188.067° SSW | 25.481° | 2025-11-09 12:07:19.700Z | 146.202° SSE |
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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