STARLINK-1714, 46562
Orbit data source: Space-Track
STARLINK-1714, 46562 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 06 Oct 2020 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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46562 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Partially operational Commercial Communications
Bus & Motor
STARLINK, Unknown motor
Mass
260 kg wet, ~248 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 10.1 m
Radar Cross Section
13.562 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 STARLINK-1714
1 46562U 20070AG 25293.66671296 .00104382 00000-0 39372-2 0 9990
2 46562 53.0565 55.6130 0003932 117.1538 309.9338 15.26214530 5540Epoch: 2025-10-20T16:00Z
TLE epoch observation values (Epoch: 2025-10-20T16:00:03.999Z)
Latitude
47.53602°
Longitude
-158.9665°
Altitude
490.657 km
Speed
7.626 km/s
True Right ascension
07h 21m 39s
True Declination
47° 21' 29"
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
21:15:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
490.113 km
Perigee altitude
484.714 km
Semi-major axis
6,865.551 km
Eccentricity
0.00039
Inclination
53.0565°
RAAN
55.613°
Arg. of periapsis
117.1538°
True anomaly
309.89924°
Mean anomaly
309.9338°
Eccentric anomaly
309.91652°
Mean motion
3.81531 °/min
Orbital period
94.36 mins
BSTAR
0.0039372
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Other satellites on launch #70 in the year 2020 (2020-10-06 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-1714 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-21 10:43:55.822Z | 217.887° SW | 2025-10-21 10:46:55.822Z | 177.816° S | 39.981° | 2025-10-21 10:50:55.822Z | 56.041° ENE |
| 4 mins | 2025-10-21 12:23:55.822Z | 294.566° NW | 2025-10-21 12:25:55.822Z | 337.227° NNW | 20.827° | 2025-10-21 12:27:55.822Z | 17.871° NNE |
| 6 mins | 2025-10-21 17:20:55.822Z | 321.772° NNW | 2025-10-21 17:23:55.822Z | 71.631° E | 37.896° | 2025-10-21 17:26:55.822Z | 115.748° SE |
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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