DECAYED

STARLINK-31894, 59665 (Decayed)

Orbit data source: Space-Track

STARLINK-31894, 59665 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 06 May 2024 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-31894 details

Identifier	59665, 2024-084M
Orbit	Decayed
Last TLE update	3 months ago
Origin	SpaceX/Seattle (US)
Manufacturer	SpaceX/Seattle
Mission	Decayed spacecraft
Bus & Motor	STARLINK V2M, Unknown motor
Mass	730 kg wet, ~700 kg dry
Launch date (UTC)	2024-05-06 (8 months ago)
Launch vehicle	FALCON 9
Launch site	Air Force Eastern Test Range (AFETR)
Object type	Payload Rocket body Debris
Shape & HBR	Unknown
Radar Cross Section	Large (>1 m²)

Expand to show TLE details & history

TLE from 3 months ago

0 STARLINK-31894
1 59665U 24084M   24263.09663046  .09667759  90625-5  20651-2 0  9992
2 59665  42.9799 180.3365 0006562 252.7832 240.2526 16.29697157 22409

Epoch: 2024-09-19T02:19Z

Definitive object data (Epoch: 2024-09-19T02:19:08.871Z)

Latitude	30.04023°
Longitude	-71.03636°
Altitude	196.03 km
Speed	7.792 km/s
True Right ascension	21h 28m 57s
True Declination	29° 52' 43"
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	199.701 km
Perigee altitude	191.074 km
Semi-major axis	6,573.525 km
Eccentricity	0.0006562
Inclination	42.9799°
RAAN	180.3365°
Arg. of periapsis	252.7832°
True anomaly	240.18734°
Mean anomaly	240.2526°
Eccentric anomaly	240.21997°
Mean motion	4.07236 °/min
BSTAR	0.0020651
Orbital period	88.4 mins