DECAYED

STARLINK-1509, 45766 (Decayed)

Orbit data source: Space-Track

STARLINK-1509, 45766 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-1509 details

Identifier	45766, 2020-038AN
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-1509
1 45766U 20038AN  24329.58639442  .12678913  12479-4  55143-3 0  9997
2 45766  53.0176  24.3587 0000748  35.7308 119.3222 16.43828378248549

Epoch: 2024-11-24T14:04Z

Definitive object data (Epoch: 2024-11-24T14:04:24.477Z)

Latitude	19.72697°
Longitude	-86.3402°
Altitude	156.335 km
Speed	7.815 km/s
True Right ascension	12h 35m 08s
True Declination	19° 36' 29"
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	156.42 km
Perigee altitude	155.442 km
Semi-major axis	6,534.068 km
Eccentricity	0.0000748
Inclination	53.0176°
RAAN	24.3587°
Arg. of periapsis	35.7308°
True anomaly	119.32967°
Mean anomaly	119.3222°
Eccentric anomaly	119.32594°
Mean motion	4.1093 °/min
BSTAR	0.00055143
Orbital period	87.61 mins