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: 8 hours ago
TLE from 8 hours ago
0 STARLINK-1714
1 46562U 20070AG 25346.95739078 .00099621 00000-0 29654-2 0 9995
2 46562 53.0525 167.5444 0006683 141.8940 218.2535 15.33900847286974Epoch: 2025-12-12T22:58Z
TLE epoch observation values (Epoch: 2025-12-12T22:58:38.563Z)
Latitude
0.00001°
Longitude
100.99217°
Altitude
468.669 km
Speed
7.631 km/s
True Right ascension
11h 10m 10s
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
05:21:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
469.034 km
Perigee altitude
459.889 km
Semi-major axis
6,842.598 km
Eccentricity
0.00067
Inclination
53.0525°
RAAN
167.5444°
Arg. of periapsis
141.894°
True anomaly
218.20612°
Mean anomaly
218.2535°
Eccentric anomaly
218.22981°
Mean motion
3.83453 °/min
Orbital period
93.88 mins
BSTAR
0.0029654
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-13 14:47:31.814Z | 217.843° SW | 2025-12-13 14:50:31.814Z | 103.766° ESE | 41.681° | 2025-12-13 14:53:31.814Z | 55.547° ENE |
| 4 mins | 2025-12-13 16:26:31.814Z | 299.266° NW | 2025-12-13 16:28:31.814Z | 343.641° N | 19.361° | 2025-12-13 16:30:31.814Z | 21.146° NNE |
| 5 mins | 2025-12-13 21:22:31.814Z | 328.306° NNW | 2025-12-13 21:24:31.814Z | 60.628° ENE | 38.858° | 2025-12-13 21:27:31.814Z | 115.526° 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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