DECAYED

STARLINK-1126, 44951 (Decayed)

Orbit data source: Space-Track

STARLINK-1126, 44951 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-1126 details

Identifier	44951, 2020-001AP
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-1126
1 44951U 20001AP  24135.78744387  .17366604  12163-4  35623-2 0  9990
2 44951  52.9854 234.0743 0005953 308.2104 191.2171 16.30377494243916

Epoch: 2024-05-14T18:53Z

Definitive object data (Epoch: 2024-05-14T18:53:55.15Z)

Latitude	31.40066°
Longitude	-129.64262°
Altitude	197.273 km
Speed	7.79 km/s
True Right ascension	01h 47m 22s
True Declination	31° 14' 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	195.733 km
Perigee altitude	187.911 km
Semi-major axis	6,569.959 km
Eccentricity	0.0005953
Inclination	52.9854°
RAAN	234.0743°
Arg. of periapsis	308.2104°
True anomaly	191.20384°
Mean anomaly	191.2171°
Eccentric anomaly	191.21047°
Mean motion	4.07567 °/min
BSTAR	0.0035623
Orbital period	88.33 mins