DECAYED

STARLINK-1906, 46765 (Decayed)

Orbit data source: Space-Track

STARLINK-1906, 46765 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 24 Oct 2020 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payloads include a variety of satellites, spacecraft, and rockets 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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Identifier	46765, 2020-074AC
Orbit	Decayed
Last TLE update	1 month ago
Origin	SpaceX/Seattle (US)
Manufacturer	SpaceX/Seattle
Mission	Decayed Commercial Communications
Bus & Motor	STARLINK, Unknown motor
Mass	260 kg wet, ~248 kg dry
Launch date (UTC)	2020-10-24 (4 years ago)
Launch vehicle	FALCON 9
Launch site	Air Force Eastern Test Range (AFETR)
Object type	Payload Rocket body Debris
Shape & HBR	Box + 1 Pan, 10.11 m
Radar Cross Section	13.562 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 month ago

0 STARLINK-1906
1 46765U 20074AC  25056.69233987  .11002963  12415-4  91567-3 0  9996
2 46765  53.0328 178.8714 0007789 311.5506 188.5221 16.38797151240066

Epoch: 2025-02-25T16:36Z

Definitive object data (Epoch: 2025-02-25T16:36:58.164Z)

Latitude	30.96128°
Longitude	-72.84012°
Altitude	175.891 km
Speed	7.802 km/s
True Right ascension	22h 08m 46s
True Declination	30° 47' 47"
Sunlit	Object was in daylight at TLE epoch

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Orbital elements

Apogee altitude	174.394 km
Perigee altitude	164.194 km
Semi-major axis	6,547.431 km
Eccentricity	0.0007789
Inclination	53.0328°
RAAN	178.8714°
Arg. of periapsis	311.5506°
True anomaly	188.50889°
Mean anomaly	188.5221°
Eccentric anomaly	188.51549°
Mean motion	4.09672 °/min
BSTAR	0.00091567
Orbital period	87.88 mins