DECAYED

STARLINK-1442, 45659 (Decayed)

Orbit data source: Space-Track

STARLINK-1442, 45659 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 04 Jun 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-1442 details

Identifier	45659, 2020-035C
Orbit	Decayed
Last TLE update	6 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)	2020-06-04 (4 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 6 months ago

0 STARLINK-1442
1 45659U 20035C   24161.15274425  .21355086  12157-4  31812-2 0  9990
2 45659  53.0303   1.9468 0010725 262.1622 204.0290 16.33440417222791

Epoch: 2024-06-09T03:39Z

Definitive object data (Epoch: 2024-06-09T03:39:57.103Z)

Latitude	50.28163°
Longitude	164.67867°
Altitude	195.564 km
Speed	7.792 km/s
True Right ascension	07h 50m 41s
True Declination	50° 05' 53"
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	190.637 km
Perigee altitude	176.562 km
Semi-major axis	6,561.737 km
Eccentricity	0.0010725
Inclination	53.0303°
RAAN	1.9468°
Arg. of periapsis	262.1622°
True anomaly	203.97902°
Mean anomaly	204.029°
Eccentric anomaly	204.004°
Mean motion	4.08333 °/min
BSTAR	0.0031812
Orbital period	88.16 mins