DECAYED

STARLINK-1120, 45045 (Decayed)

Orbit data source: Space-Track

STARLINK-1120, 45045 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-1120 details

Identifier	45045, 2020-006B
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-1120
1 45045U 20006B   24176.48747890  .14269972  12056-4  30744-2 0  9991
2 45045  53.0323 146.4963 0001758 169.8801 290.6673 16.29920872243674

Epoch: 2024-06-24T11:41Z

Definitive object data (Epoch: 2024-06-24T11:41:58.176Z)

Latitude	51.9262°
Longitude	165.07579°
Altitude	198.544 km
Speed	7.794 km/s
True Right ascension	16h 54m 45s
True Declination	51° 44' 42"
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	194.196 km
Perigee altitude	191.886 km
Semi-major axis	6,571.178 km
Eccentricity	0.0001758
Inclination	53.0323°
RAAN	146.4963°
Arg. of periapsis	169.8801°
True anomaly	290.64845°
Mean anomaly	290.6673°
Eccentric anomaly	290.65788°
Mean motion	4.07454 °/min
BSTAR	0.0030744
Orbital period	88.35 mins