DECAYED

STARLINK-1467, 45733 (Decayed)

Orbit data source: Space-Track

STARLINK-1467, 45733 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-1467 details

Identifier	45733, 2020-038D
Orbit	Decayed
Last TLE update	1 month 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 1 month ago

0 STARLINK-1467
1 45733U 20038D   24328.74756175  .21316887  12646-4  41283-3 0  9996
2 45733  53.0416  57.2505 0005261 359.0237 143.8585 16.47005152248212

Epoch: 2024-11-23T17:56Z

Definitive object data (Epoch: 2024-11-23T17:56:29.335Z)

Latitude	28.89595°
Longitude	-119.45446°
Altitude	151.526 km
Speed	7.818 km/s
True Right ascension	14h 11m 27s
True Declination	28° 44' 14"
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	150.956 km
Perigee altitude	144.09 km
Semi-major axis	6,525.66 km
Eccentricity	0.0005261
Inclination	53.0416°
RAAN	57.2505°
Arg. of periapsis	359.0237°
True anomaly	143.89404°
Mean anomaly	143.8585°
Eccentric anomaly	143.87627°
Mean motion	4.11724 °/min
BSTAR	0.00041283
Orbital period	87.44 mins