DECAYED

STARLINK-1783, 46686 (Decayed)

Orbit data source: Space-Track

STARLINK-1783, 46686 was 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). 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.

Not visible in the next 10 days

STARLINK-1783 details

Identifier	46686, 2020-073S
Orbit	Decayed
Last TLE update	6 months 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)	2020-10-18 (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, 8.86 m
Radar Cross Section	13.562 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 6 months ago

0 STARLINK-1783
1 46686U 20073S   24160.62730618  .11860947  11933-4  45736-2 0  9992
2 46686  53.0447 211.0661 0002354 313.0057 186.0218 16.23328042201555

Epoch: 2024-06-08T15:03Z

Definitive object data (Epoch: 2024-06-08T15:03:19.253Z)

Latitude	31.70518°
Longitude	-119.77469°
Altitude	214.043 km
Speed	7.782 km/s
True Right ascension	00h 14m 10s
True Declination	31° 32' 20"
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	212.368 km
Perigee altitude	209.266 km
Semi-major axis	6,588.954 km
Eccentricity	0.0002354
Inclination	53.0447°
RAAN	211.0661°
Arg. of periapsis	313.0057°
True anomaly	186.01897°
Mean anomaly	186.0218°
Eccentric anomaly	186.02039°
Mean motion	4.05806 °/min
BSTAR	0.0045736
Orbital period	88.71 mins