DECAYED

STARLINK-1377, 45547 (Decayed)

Orbit data source: Space-Track

STARLINK-1377, 45547 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 22 Apr 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-1377 details

Identifier	45547, 2020-025S
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)	2020-04-22 (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 3 months ago

0 STARLINK-1377
1 45547U 20025S   24252.68243785  .23606485  12278-4  39847-2 0  9993
2 45547  53.0274 319.4864 0008025 338.5560 160.5969 16.32311541243178

Epoch: 2024-09-08T16:22Z

Definitive object data (Epoch: 2024-09-08T16:22:42.63Z)

Latitude	31.58444°
Longitude	-121.81348°
Altitude	193.251 km
Speed	7.792 km/s
True Right ascension	07h 28m 20s
True Declination	31° 25' 05"
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	191.893 km
Perigee altitude	181.357 km
Semi-major axis	6,564.762 km
Eccentricity	0.0008025
Inclination	53.0274°
RAAN	319.4864°
Arg. of periapsis	338.556°
True anomaly	160.62742°
Mean anomaly	160.5969°
Eccentric anomaly	160.61216°
Mean motion	4.08051 °/min
BSTAR	0.0039847
Orbital period	88.22 mins