DECAYED

STARLINK-1289, 45391 (Decayed)

Orbit data source: Space-Track

STARLINK-1289, 45391 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-1289 details

Identifier	45391, 2020-019AH
Orbit	Decayed
Last TLE update	3 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 3 months ago

0 STARLINK-1289
1 45391U 20019AH  24270.40371150  .30193633  12506-4  11446-2 0  9994
2 45391  53.0436 331.1713 0010196 288.8932 181.2948 16.43234845250382

Epoch: 2024-09-26T09:41Z

Definitive object data (Epoch: 2024-09-26T09:41:20.673Z)

Latitude	48.74555°
Longitude	-58.37588°
Altitude	169.349 km
Speed	7.807 km/s
True Right ascension	06h 10m 35s
True Declination	48° 33' 35"
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	164.163 km
Perigee altitude	150.836 km
Semi-major axis	6,535.637 km
Eccentricity	0.0010196
Inclination	53.0436°
RAAN	331.1713°
Arg. of periapsis	288.8932°
True anomaly	181.29216°
Mean anomaly	181.2948°
Eccentric anomaly	181.29348°
Mean motion	4.10782 °/min
BSTAR	0.0011446
Orbital period	87.64 mins