DECAYED

STARLINK-1344, 45559 (Decayed)

Orbit data source: Space-Track

STARLINK-1344, 45559 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-1344 details

Identifier	45559, 2020-025AE
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-1344
1 45559U 20025AE  24263.23564557  .50767146  12444-4  28122-2 0  9993
2 45559  53.0305 261.0035 0002167 317.5301 151.2564 16.42191516244942

Epoch: 2024-09-19T05:39Z

Definitive object data (Epoch: 2024-09-19T05:39:19.777Z)

Latitude	49.29724°
Longitude	-62.9115°
Altitude	166.821 km
Speed	7.812 km/s
True Right ascension	01h 22m 10s
True Declination	49° 06' 42"
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	161.686 km
Perigee altitude	158.853 km
Semi-major axis	6,538.407 km
Eccentricity	0.0002167
Inclination	53.0305°
RAAN	261.0035°
Arg. of periapsis	317.5301°
True anomaly	151.26834°
Mean anomaly	151.2564°
Eccentric anomaly	151.26237°
Mean motion	4.10521 °/min
BSTAR	0.0028122
Orbital period	87.69 mins