DECAYED

STARLINK-1149, 45079 (Decayed)

Orbit data source: Space-Track

STARLINK-1149, 45079 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 29 Jan 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-1149 details

Identifier	45079, 2020-006AM
Orbit	Decayed
Last TLE update	6 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)	2020-01-29 (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 6 months ago

0 STARLINK-1149
1 45079U 20006AM  24181.11001221  .23179628  12110-4  42270-2 0  9991
2 45079  53.0321 116.1377 0005347 256.3400 235.4724 16.31600972244143

Epoch: 2024-06-29T02:38Z

Definitive object data (Epoch: 2024-06-29T02:38:25.054Z)

Latitude	36.70581°
Longitude	-55.05684°
Altitude	193.119 km
Speed	7.794 km/s
True Right ascension	17h 28m 54s
True Declination	36° 31' 37"
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	192.041 km
Perigee altitude	185.019 km
Semi-major axis	6,566.667 km
Eccentricity	0.0005347
Inclination	53.0321°
RAAN	116.1377°
Arg. of periapsis	256.34°
True anomaly	235.42194°
Mean anomaly	235.4724°
Eccentric anomaly	235.44717°
Mean motion	4.07874 °/min
BSTAR	0.004227
Orbital period	88.26 mins