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, 4.4 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 25259.60071076 .00057426 00000-0 25640-2 0 9995
2 46562 53.0496 212.5459 0008790 12.0414 348.0790 15.20805121273622Epoch: 2025-09-16T14:25Z
TLE epoch observation values (Epoch: 2025-09-16T14:25:01.409Z)
Latitude
-0.00001°
Longitude
0.50134°
Altitude
498.377 km
Speed
7.62 km/s
True Right ascension
14h 10m 11s
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
14:47:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.733 km
Perigee altitude
497.635 km
Semi-major axis
6,881.821 km
Eccentricity
0.00088
Inclination
53.0496°
RAAN
212.5459°
Arg. of periapsis
12.0414°
True anomaly
348.05817°
Mean anomaly
348.079°
Eccentric anomaly
348.06859°
Mean motion
3.80179 °/min
Orbital period
94.69 mins
BSTAR
0.002564
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-17 00:05:26.913Z | 244.351° WSW | 2025-09-17 00:07:26.913Z | 340.227° N | 42.924° | 2025-09-17 00:10:26.913Z | 44.867° NE |
| 4 mins | 2025-09-17 05:04:26.913Z | 351.367° N | 2025-09-17 05:06:26.913Z | 34.36° NE | 19.56° | 2025-09-17 05:08:26.913Z | 69.198° E |
| 6 mins | 2025-09-17 06:42:26.913Z | 305.04° NW | 2025-09-17 06:44:26.913Z | 279.778° WNW | 42.407° | 2025-09-17 06:48:26.913Z | 136.463° 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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