STARLINK-1716, 46672
Orbit data source: Space-Track
STARLINK-1716, 46672 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 18 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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46672 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: 6 hours ago
TLE from 6 hours ago
0 STARLINK-1716
1 46672U 20073C 26026.66667824 .00114779 00000-0 18893-2 0 9998
2 46672 53.0491 45.3001 0005394 243.9637 111.2217 15.51484080 5924Epoch: 2026-01-26T16:00Z
TLE epoch observation values (Epoch: 2026-01-26T16:00:00.999Z)
Latitude
-3.90427°
Longitude
36.41051°
Altitude
415.205 km
Speed
7.662 km/s
True Right ascension
02h 49m 29s
True Declination
-3° 52' 47"
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
23:36:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
416.332 km
Perigee altitude
409.006 km
Semi-major axis
6,790.806 km
Eccentricity
0.00054
Inclination
53.0491°
RAAN
45.3001°
Arg. of periapsis
243.9637°
True anomaly
111.27931°
Mean anomaly
111.2217°
Eccentric anomaly
111.2505°
Mean motion
3.87848 °/min
Orbital period
92.82 mins
BSTAR
0.0018893
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Other satellites on launch #73 in the year 2020 (2020-10-18 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-1716 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 | 2026-01-27 03:00:02.645Z | 175.602° S | 2026-01-27 03:02:02.645Z | 134.189° SE | 19.199° | 2026-01-27 03:04:02.645Z | 89.04° E |
| 4 mins | 2026-01-27 04:37:02.645Z | 272.641° WNW | 2026-01-27 04:38:02.645Z | 302.359° NW | 30.598° | 2026-01-27 04:41:02.645Z | 32.809° NE |
| 4 mins | 2026-01-27 11:06:02.645Z | 290.162° WNW | 2026-01-27 11:08:02.645Z | 210.497° SW | 36.559° | 2026-01-27 11:10:02.645Z | 154.413° 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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