DECAYED

STARLINK-1499, 45762 (Decayed)

Orbit data source: Space-Track

STARLINK-1499, 45762 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

STARLINK-1499 details

Identifier	45762, 2020-038AJ
Orbit	Decayed
Last TLE update	1 week 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, 8.86 m
Radar Cross Section	13.562 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 week ago

0 STARLINK-1499
1 45762U 20038AJ  24353.81353719  .29218038  12620-4  23623-3 0  9998
2 45762  52.9771 272.6018 0005231 201.4755 262.6541 16.51974855252228

Epoch: 2024-12-18T19:31Z

Definitive object data (Epoch: 2024-12-18T19:31:29.613Z)

Latitude	50.91192°
Longitude	4.44975°
Altitude	140.531 km
Speed	7.828 km/s
True Right ascension	01h 40m 54s
True Declination	50° 43' 39"
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	137.848 km
Perigee altitude	131.034 km
Semi-major axis	6,512.578 km
Eccentricity	0.0005231
Inclination	52.9771°
RAAN	272.6018°
Arg. of periapsis	201.4755°
True anomaly	262.59465°
Mean anomaly	262.6541°
Eccentric anomaly	262.62438°
Mean motion	4.12966 °/min
BSTAR	0.00023623
Orbital period	87.17 mins