DECAYED

STARLINK-1461, 45730 (Decayed)

Orbit data source: Space-Track

STARLINK-1461, 45730 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 13 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-1461 details

Identifier	45730, 2020-038A
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)	2020-06-13 (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-1461
1 45730U 20038A   24236.87440228  .42894763  12405-4  99483-3 0  9999
2 45730  53.0197 182.0686 0009579 220.2987 235.3561 16.45627210233307

Epoch: 2024-08-23T20:59Z

Definitive object data (Epoch: 2024-08-23T20:59:08.356Z)

Latitude	52.82128°
Longitude	-6.14748°
Altitude	160.826 km
Speed	7.814 km/s
True Right ascension	18h 45m 06s
True Declination	52° 38' 25"
Sunlit	Object was in partial 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	157.423 km
Perigee altitude	144.914 km
Semi-major axis	6,529.306 km
Eccentricity	0.0009579
Inclination	53.0197°
RAAN	182.0686°
Arg. of periapsis	220.2987°
True anomaly	235.26586°
Mean anomaly	235.3561°
Eccentric anomaly	235.31097°
Mean motion	4.1138 °/min
BSTAR	0.00099483
Orbital period	87.51 mins