DECAYED

STARLINK-1486, 45757 (Decayed)

Orbit data source: Space-Track

STARLINK-1486, 45757 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 13 Jun 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

Identifier	45757, 2020-038AD
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)	2020-06-13 (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, 10.11 m
Radar Cross Section	13.562 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 3 months ago

0 STARLINK-1486
1 45757U 20038AD  25004.04580993  .12121608  12413-4  49660-3 0  9994
2 45757  53.0411 221.1695 0005572 241.4495 241.1901 16.43497623254596

Epoch: 2025-01-04T01:05Z

Definitive object data (Epoch: 2025-01-04T01:05:57.977Z)

Latitude	42.46409°
Longitude	-122.43117°
Altitude	162.351 km
Speed	7.813 km/s
True Right ascension	23h 51m 50s
True Declination	42° 16' 38"
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	160.445 km
Perigee altitude	153.162 km
Semi-major axis	6,534.941 km
Eccentricity	0.0005572
Inclination	53.0411°
RAAN	221.1695°
Arg. of periapsis	241.4495°
True anomaly	241.13417°
Mean anomaly	241.1901°
Eccentric anomaly	241.16213°
Mean motion	4.10848 °/min
BSTAR	0.0004966
Orbital period	87.62 mins