DECAYED

STARLINK-1110, 44946 (Decayed)

Orbit data source: Space-Track

STARLINK-1110, 44946 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-1110 details

Identifier	44946, 2020-001AJ
Orbit	Decayed
Last TLE update	9 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 9 months ago

0 STARLINK-1110
1 44946U 20001AJ  24101.30511192  .09874184  11821-4  44382-2 0  9991
2 44946  52.9924  47.4575 0002378 194.8867 193.8851 16.21437839237242

Epoch: 2024-04-10T07:19Z

Definitive object data (Epoch: 2024-04-10T07:19:21.669Z)

Latitude	22.65854°
Longitude	116.83112°
Altitude	217.886 km
Speed	7.778 km/s
True Right ascension	04h 22m 45s
True Declination	22° 31' 36"
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	217.513 km
Perigee altitude	214.377 km
Semi-major axis	6,594.082 km
Eccentricity	0.0002378
Inclination	52.9924°
RAAN	47.4575°
Arg. of periapsis	194.8867°
True anomaly	193.87856°
Mean anomaly	193.8851°
Eccentric anomaly	193.88183°
Mean motion	4.05333 °/min
BSTAR	0.0044382
Orbital period	88.82 mins