DECAYED

STARLINK-1140, 45050 (Decayed)

Orbit data source: Space-Track

STARLINK-1140, 45050 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 29 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-1140 details

Identifier	45050, 2020-006G
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)	2020-01-29 (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-1140
1 45050U 20006G   24227.19849287  .33502581  12354-4  31626-2 0  9993
2 45050  53.0265 263.7698 0005285 307.4262 173.5243 16.37789644251493

Epoch: 2024-08-14T04:45Z

Definitive object data (Epoch: 2024-08-14T04:45:49.783Z)

Latitude	43.38801°
Longitude	4.17368°
Altitude	179.409 km
Speed	7.802 km/s
True Right ascension	02h 34m 56s
True Declination	43° 12' 04"
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	175.441 km
Perigee altitude	168.518 km
Semi-major axis	6,550.116 km
Eccentricity	0.0005285
Inclination	53.0265°
RAAN	263.7698°
Arg. of periapsis	307.4262°
True anomaly	173.53113°
Mean anomaly	173.5243°
Eccentric anomaly	173.52771°
Mean motion	4.09421 °/min
BSTAR	0.0031626
Orbital period	87.93 mins