DECAYED

STARLINK-1083, 44939 (Decayed)

Orbit data source: Space-Track

STARLINK-1083, 44939 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 07 Jan 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-1083 details

Identifier	44939, 2020-001AB
Orbit	Decayed
Last TLE update	4 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)	2020-01-07 (5 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 4 months ago

0 STARLINK-1083
1 44939U 20001AB  24240.51923502  .18977761  12156-4  37563-2 0  9992
2 44939  53.0333 255.5186 0003183  28.5359 106.6668 16.30794940256680

Epoch: 2024-08-27T12:27Z

Definitive object data (Epoch: 2024-08-27T12:27:41.905Z)

Latitude	34.35257°
Longitude	-118.40258°
Altitude	193.443 km
Speed	7.795 km/s
True Right ascension	02h 59m 01s
True Declination	34° 10' 44"
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	192.784 km
Perigee altitude	188.602 km
Semi-major axis	6,568.83 km
Eccentricity	0.0003183
Inclination	53.0333°
RAAN	255.5186°
Arg. of periapsis	28.5359°
True anomaly	106.70174°
Mean anomaly	106.6668°
Eccentric anomaly	106.68427°
Mean motion	4.07672 °/min
BSTAR	0.0037563
Orbital period	88.31 mins