DECAYED

STARLINK-1396, 45681 (Decayed)

Orbit data source: Space-Track

STARLINK-1396, 45681 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 04 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-1396 details

Identifier	45681, 2020-035AA
Orbit	Decayed
Last TLE update	6 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)	2020-06-04 (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 6 months ago

0 STARLINK-1396
1 45681U 20035AA  24188.41185093  .20957709  12377-4  19423-2 0  9992
2 45681  53.0136 229.7481 0005246 322.1080  52.9322 16.37950032227044

Epoch: 2024-07-06T09:53Z

Definitive object data (Epoch: 2024-07-06T09:53:03.92Z)

Latitude	11.99569°
Longitude	165.76258°
Altitude	169.345 km
Speed	7.808 km/s
True Right ascension	15h 55m 36s
True Declination	11° 55' 11"
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	174.99 km
Perigee altitude	168.118 km
Semi-major axis	6,549.691 km
Eccentricity	0.0005246
Inclination	53.0136°
RAAN	229.7481°
Arg. of periapsis	322.108°
True anomaly	52.98019°
Mean anomaly	52.9322°
Eccentric anomaly	52.95619°
Mean motion	4.0946 °/min
BSTAR	0.0019423
Orbital period	87.92 mins