DECAYED

STARLINK-1445, 45662 (Decayed)

Orbit data source: Space-Track

STARLINK-1445, 45662 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-1445 details

Identifier	45662, 2020-035F
Orbit	Decayed
Last TLE update	1 week 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 (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 1 week ago

0 STARLINK-1445
1 45662U 20035F   24353.16550904  .06726882  12189-4  85598-3 0  9992
2 45662  53.0381 237.3309 0004506 233.4481 264.8043 16.35122598251537

Epoch: 2024-12-18T03:58Z

Definitive object data (Epoch: 2024-12-18T03:58:19.981Z)

Latitude	32.28664°
Longitude	-117.72834°
Altitude	181.147 km
Speed	7.802 km/s
True Right ascension	01h 56m 28s
True Declination	32° 07' 04"
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	182.052 km
Perigee altitude	176.143 km
Semi-major axis	6,557.235 km
Eccentricity	0.0004506
Inclination	53.0381°
RAAN	237.3309°
Arg. of periapsis	233.4481°
True anomaly	264.75288°
Mean anomaly	264.8043°
Eccentric anomaly	264.77859°
Mean motion	4.08754 °/min
BSTAR	0.00085598
Orbital period	88.07 mins