DECAYED

STARLINK-1634, 46152 (Decayed)

Orbit data source: Space-Track

STARLINK-1634, 46152 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 18 Aug 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-1634 details

Identifier	46152, 2020-057AM
Orbit	Decayed
Last TLE update	4 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)	2020-08-18 (4 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 4 months ago

0 STARLINK-1634
1 46152U 20057AM  24248.55194535  .13201841  11964-4  46288-2 0  9994
2 46152  53.0327 228.5099 0003621  63.6457  41.6627 16.24454441224243

Epoch: 2024-09-04T13:14Z

Definitive object data (Epoch: 2024-09-04T13:14:48.078Z)

Latitude	50.55681°
Longitude	160.19963°
Altitude	211.596 km
Speed	7.787 km/s
True Right ascension	22h 52m 12s
True Declination	50° 22' 26"
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	210.158 km
Perigee altitude	205.388 km
Semi-major axis	6,585.91 km
Eccentricity	0.0003621
Inclination	53.0327°
RAAN	228.5099°
Arg. of periapsis	63.6457°
True anomaly	41.69029°
Mean anomaly	41.6627°
Eccentric anomaly	41.6765°
Mean motion	4.06087 °/min
BSTAR	0.0046288
Orbital period	88.65 mins