DECAYED

STARLINK-1287, 45371 (Decayed)

Orbit data source: Space-Track

STARLINK-1287, 45371 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-1287 details

Identifier	45371, 2020-019M
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)	2020-03-18 (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 4 months ago

0 STARLINK-1287
1 45371U 20019M   24230.01005044  .20361866  12051-4  45053-2 0  9991
2 45371  53.0348 132.4947 0007924 259.7910 201.8269 16.29533865244859

Epoch: 2024-08-17T00:14Z

Definitive object data (Epoch: 2024-08-17T00:14:28.358Z)

Latitude	51.66753°
Longitude	-88.15483°
Altitude	204.768 km
Speed	7.787 km/s
True Right ascension	16h 05m 21s
True Declination	51° 29' 10"
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	199.289 km
Perigee altitude	188.873 km
Semi-major axis	6,572.218 km
Eccentricity	0.0007924
Inclination	53.0348°
RAAN	132.4947°
Arg. of periapsis	259.791°
True anomaly	201.79317°
Mean anomaly	201.8269°
Eccentric anomaly	201.81003°
Mean motion	4.07357 °/min
BSTAR	0.0045053
Orbital period	88.37 mins