DECAYED

STARLINK-1584, 46044 (Decayed)

Orbit data source: Space-Track

STARLINK-1584, 46044 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Fri, 07 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

Identifier	46044, 2020-055T
Orbit	Decayed
Last TLE update	10 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)	2020-08-07 (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 10 months ago

0 STARLINK-1584
1 46044U 20055T   24145.14838534  .26651884  12301-4  34690-2 0  9997
2 46044  53.0346 154.1790 0005068 338.7965 140.0746 16.34896364210159

Epoch: 2024-05-24T03:33Z

Definitive object data (Epoch: 2024-05-24T03:33:40.493Z)

Latitude	44.52819°
Longitude	-8.86897°
Altitude	186.497 km
Speed	7.799 km/s
True Right ascension	19h 07m 07s
True Declination	44° 20' 29"
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	183.027 km
Perigee altitude	176.379 km
Semi-major axis	6,557.84 km
Eccentricity	0.0005068
Inclination	53.0346°
RAAN	154.179°
Arg. of periapsis	338.7965°
True anomaly	140.11185°
Mean anomaly	140.0746°
Eccentric anomaly	140.09323°
Mean motion	4.08697 °/min
BSTAR	0.003469
Orbital period	88.08 mins