DECAYED

STARLINK-1119, 44928 (Decayed)

Orbit data source: Space-Track

STARLINK-1119, 44928 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-1119 details

Identifier	44928, 2020-001Q
Orbit	Decayed
Last TLE update	7 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 7 months ago

0 STARLINK-1119
1 44928U 20001Q   24136.08916718  .17779497  12124-4  38190-2 0  9994
2 44928  53.0443   3.6776 0007991 287.9366 247.4073 16.29846001240969

Epoch: 2024-05-15T02:08Z

Definitive object data (Epoch: 2024-05-15T02:08:24.044Z)

Latitude	3.72751°
Longitude	-84.51882°
Altitude	195.492 km
Speed	7.789 km/s
True Right ascension	12h 03m 32s
True Declination	3° 42' 12"
Sunlit	Object was in full shadow 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	198.491 km
Perigee altitude	187.989 km
Semi-major axis	6,571.377 km
Eccentricity	0.0007991
Inclination	53.0443°
RAAN	3.6776°
Arg. of periapsis	287.9366°
True anomaly	247.32279°
Mean anomaly	247.4073°
Eccentric anomaly	247.36504°
Mean motion	4.07435 °/min
BSTAR	0.003819
Orbital period	88.36 mins