DECAYED

STARLINK-1100, 44943 (Decayed)

Orbit data source: Space-Track

STARLINK-1100, 44943 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-1100 details

Identifier	44943, 2020-001AF
Orbit	Decayed
Last TLE update	4 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 4 months ago

0 STARLINK-1100
1 44943U 20001AF  24229.39749808  .33137268  12409-4  25993-2 0  9997
2 44943  53.0256 289.2103 0004082 344.2138 122.2916 16.39387773255235

Epoch: 2024-08-16T09:32Z

Definitive object data (Epoch: 2024-08-16T09:32:23.834Z)

Latitude	50.13635°
Longitude	-62.84735°
Altitude	174.65 km
Speed	7.807 km/s
True Right ascension	03h 02m 05s
True Declination	49° 57' 07"
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	170.394 km
Perigee altitude	165.05 km
Semi-major axis	6,545.859 km
Eccentricity	0.0004082
Inclination	53.0256°
RAAN	289.2103°
Arg. of periapsis	344.2138°
True anomaly	122.33113°
Mean anomaly	122.2916°
Eccentric anomaly	122.31137°
Mean motion	4.0982 °/min
BSTAR	0.0025993
Orbital period	87.84 mins