DECAYED

STARLINK-1160, 45082 (Decayed)

Orbit data source: Space-Track

STARLINK-1160, 45082 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-1160 details

Identifier	45082, 2020-006AQ
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)	2020-01-29 (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 3 months ago

0 STARLINK-1160
1 45082U 20006AQ  24256.06219858  .11579768  11918-4  46324-2 0  9994
2 45082  53.0331 101.1880 0009755 280.3721 215.5097 16.22746085256333

Epoch: 2024-09-12T01:29Z

Definitive object data (Epoch: 2024-09-12T01:29:33.957Z)

Latitude	33.95186°
Longitude	-123.01266°
Altitude	219.706 km
Speed	7.776 km/s
True Right ascension	16h 43m 43s
True Declination	33° 46' 47"
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	218.823 km
Perigee altitude	205.965 km
Semi-major axis	6,590.531 km
Eccentricity	0.0009755
Inclination	53.0331°
RAAN	101.188°
Arg. of periapsis	280.3721°
True anomaly	215.44484°
Mean anomaly	215.5097°
Eccentric anomaly	215.47726°
Mean motion	4.0566 °/min
BSTAR	0.0046324
Orbital period	88.74 mins