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: 18 hours ago
TLE from 18 hours ago
0 STARLINK-1714
1 46562U 20070AG 25353.79673738 .00069183 00000-0 20067-2 0 9994
2 46562 53.0526 135.4950 0004142 166.9745 193.1364 15.34909790288026Epoch: 2025-12-19T19:07Z
TLE epoch observation values (Epoch: 2025-12-19T19:07:18.109Z)
Latitude
-0.00004°
Longitude
120.03677°
Altitude
464.837 km
Speed
7.634 km/s
True Right ascension
09h 01m 58s
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
11:35:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.296 km
Perigee altitude
458.63 km
Semi-major axis
6,839.6 km
Eccentricity
0.00041
Inclination
53.0526°
RAAN
135.495°
Arg. of periapsis
166.9745°
True anomaly
193.12562°
Mean anomaly
193.1364°
Eccentric anomaly
193.13101°
Mean motion
3.83705 °/min
Orbital period
93.82 mins
BSTAR
0.0020067
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-20 14:08:32.900Z | 298.035° NW | 2025-12-20 14:10:32.900Z | 332.814° NNW | 16.15° | 2025-12-20 14:12:32.900Z | 11.878° NNE |
| 5 mins | 2025-12-20 19:04:32.900Z | 312.392° NW | 2025-12-20 19:06:32.900Z | 47.663° ENE | 44.861° | 2025-12-20 19:09:32.900Z | 128.373° SE |
| 6 mins | 2025-12-21 11:55:32.900Z | 224.428° SW | 2025-12-21 11:58:32.900Z | 153.243° SSE | 44.439° | 2025-12-21 12:01:32.900Z | 53.009° ENE |
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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