DECAYED

STARLINK-1450, 45667 (Decayed)

Orbit data source: Space-Track

STARLINK-1450, 45667 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-1450 details

Identifier	45667, 2020-035L
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)	2020-06-04 (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 4 months ago

0 STARLINK-1450
1 45667U 20035L   24229.93544689  .06022703  11534+0  64898-2 0  9995
2 45667  53.0376  37.8283 0012722 289.3156 209.5650 16.14963823233427

Epoch: 2024-08-16T22:27Z

Definitive object data (Epoch: 2024-08-16T22:27:02.611Z)

Latitude	31.85485°
Longitude	-112.43982°
Altitude	242.574 km
Speed	7.761 km/s
True Right ascension	12h 40m 29s
True Declination	31° 41' 20"
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	241.959 km
Perigee altitude	225.136 km
Semi-major axis	6,611.684 km
Eccentricity	0.0012722
Inclination	53.0376°
RAAN	37.8283°
Arg. of periapsis	289.3156°
True anomaly	209.49317°
Mean anomaly	209.565°
Eccentric anomaly	209.52907°
Mean motion	4.03715 °/min
BSTAR	0.0064898
Orbital period	89.17 mins