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, 14.5 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 STARLINK-11566
1 62914U 25027H 25256.25728191 .00362143 00000-0 27070-2 0 9990
2 62914 42.9982 337.4348 0000958 262.8391 97.2368 15.70817854 35282Epoch: 2025-09-13T06:10Z
TLE epoch observation values (Epoch: 2025-09-13T06:10:29.157Z)
Latitude
0.00002°
Longitude
-107.6799°
Altitude
356.411 km
Speed
7.697 km/s
True Right ascension
22h 29m 44s
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
11:36:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.186 km
Perigee altitude
357.895 km
Semi-major axis
6,736.677 km
Eccentricity
0.0001
Inclination
42.9982°
RAAN
337.4348°
Arg. of periapsis
262.8391°
True anomaly
97.24769°
Mean anomaly
97.2368°
Eccentric anomaly
97.24225°
Mean motion
3.92532 °/min
Orbital period
91.71 mins
BSTAR
0.002707
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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 | 2025-09-14 09:55:20.112Z | 263.249° W | 2025-09-14 09:56:20.112Z | 291.683° WNW | 42.458° | 2025-09-14 09:59:20.112Z | 69.883° E |
| 4 mins | 2025-09-14 11:31:20.112Z | 299.654° NW | 2025-09-14 11:33:20.112Z | 30.784° NE | 32.062° | 2025-09-14 11:35:20.112Z | 73.125° E |
| 4 mins | 2025-09-14 13:07:20.112Z | 288.621° WNW | 2025-09-14 13:09:20.112Z | 105.509° ESE | 43.538° | 2025-09-14 13:11:20.112Z | 108.484° 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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