DECAYED

STARLINK-1370, 45698 (Decayed)

Orbit data source: Space-Track

STARLINK-1370, 45698 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

Identifier	45698, 2020-035AT
Orbit	Decayed
Last TLE update	8 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, 10.11 m
Radar Cross Section	13.562 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 8 months ago

0 STARLINK-1370
1 45698U 20035AT  24209.76393478  .25793570  12122-4  33017-2 0  9992
2 45698  53.0292 101.5577 0011241 238.9908 236.2930 16.34852731230728

Epoch: 2024-07-27T18:20Z

Definitive object data (Epoch: 2024-07-27T18:20:03.964Z)

Latitude	46.45622°
Longitude	8.67029°
Altitude	188.59 km
Speed	7.797 km/s
True Right ascension	15h 18m 25s
True Declination	46° 16' 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	187.192 km
Perigee altitude	172.449 km
Semi-major axis	6,557.958 km
Eccentricity	0.0011241
Inclination	53.0292°
RAAN	101.5577°
Arg. of periapsis	238.9908°
True anomaly	236.18593°
Mean anomaly	236.293°
Eccentric anomaly	236.23945°
Mean motion	4.08686 °/min
BSTAR	0.0033017
Orbital period	88.09 mins