DECAYED

STARLINK-1108, 44944 (Decayed)

Orbit data source: Space-Track

STARLINK-1108, 44944 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 07 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-1108 details

Identifier	44944, 2020-001AG
Orbit	Decayed
Last TLE update	2 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)	2020-01-07 (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, 8.86 m
Radar Cross Section	13.562 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 2 months ago

0 STARLINK-1108
1 44944U 20001AG  24290.26573889  .15186749  12259-4  32342-2 0  9993
2 44944  53.0272  68.9234 0010605   9.1011  57.4608 16.29851318263670

Epoch: 2024-10-16T06:22Z

Definitive object data (Epoch: 2024-10-16T06:22:39.84Z)

Latitude	47.33789°
Longitude	2.30313°
Altitude	194.359 km
Speed	7.798 km/s
True Right ascension	08h 12m 56s
True Declination	47° 09' 06"
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	200.198 km
Perigee altitude	186.26 km
Semi-major axis	6,571.366 km
Eccentricity	0.0010605
Inclination	53.0272°
RAAN	68.9234°
Arg. of periapsis	9.1011°
True anomaly	57.56332°
Mean anomaly	57.4608°
Eccentric anomaly	57.51205°
Mean motion	4.07436 °/min
BSTAR	0.0032342
Orbital period	88.36 mins