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: 1 day ago
TLE from 1 day ago
0 STARLINK-11566
1 62914U 25027H 25326.00800569 .00082228 00000-0 63734-3 0 9992
2 62914 43.0007 276.9972 0001996 242.1997 117.8669 15.70863694 46253Epoch: 2025-11-22T00:11Z
TLE epoch observation values (Epoch: 2025-11-22T00:11:31.691Z)
Latitude
0.00001°
Longitude
-147.12769°
Altitude
356.827 km
Speed
7.697 km/s
True Right ascension
18h 27m 59s
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
20:51:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.753 km
Perigee altitude
357.064 km
Semi-major axis
6,736.546 km
Eccentricity
0.0002
Inclination
43.0007°
RAAN
276.9972°
Arg. of periapsis
242.1997°
True anomaly
117.88712°
Mean anomaly
117.8669°
Eccentric anomaly
117.87701°
Mean motion
3.92543 °/min
Orbital period
91.71 mins
BSTAR
0.00063734
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-23 00:50:33.686Z | 243.512° WSW | 2025-11-23 00:53:33.686Z | 136.762° SSE | 43.457° | 2025-11-23 00:55:33.686Z | 75.976° E |
| 4 mins | 2025-11-23 04:04:33.686Z | 299.341° NW | 2025-11-23 04:05:33.686Z | 327.887° NNW | 38.765° | 2025-11-23 04:08:33.686Z | 94.72° ESE |
| 4 mins | 2025-11-23 05:40:33.686Z | 255.594° W | 2025-11-23 05:41:33.686Z | 225.753° WSW | 25.237° | 2025-11-23 05:44:33.686Z | 146.48° 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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