DECAYED

STARLINK-1290, 45392 (Decayed)

Orbit data source: Space-Track

STARLINK-1290, 45392 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 18 Mar 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-1290 details

Identifier	45392, 2020-019AJ
Orbit	Decayed
Last TLE update	8 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)	2020-03-18 (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 8 months ago

0 STARLINK-1290
1 45392U 20019AJ  24123.72661051  .16261085  12726-4  14004-3 0  9998
2 45392  52.9514 113.5258 0003123 305.8063 220.6008 16.51709428230365

Epoch: 2024-05-02T17:26Z

Definitive object data (Epoch: 2024-05-02T17:26:19.148Z)

Latitude	10.81702°
Longitude	162.58355°
Altitude	136.541 km
Speed	7.826 km/s
True Right ascension	19h 01m 07s
True Declination	10° 44' 52"
Sunlit	Object was in full shadow 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	137.177 km
Perigee altitude	133.109 km
Semi-major axis	6,513.28 km
Eccentricity	0.0003123
Inclination	52.9514°
RAAN	113.5258°
Arg. of periapsis	305.8063°
True anomaly	220.57752°
Mean anomaly	220.6008°
Eccentric anomaly	220.58916°
Mean motion	4.12899 °/min
BSTAR	0.00014004
Orbital period	87.19 mins