DECAYED

STARLINK-32286, 60357 (Decayed)

Orbit data source: Space-Track

STARLINK-32286, 60357 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 04 Aug 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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-32286 details

Identifier	60357, 2024-138C
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)	2024-08-04 (5 months ago)
Launch vehicle	FALCON 9
Launch site	Air Force Western Test Range (AFWTR)
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-32286
1 60357U 24138C   24280.15845963  .06746780  12109-4  10112-2 0  9998
2 60357  53.1358 195.8207 0006605 219.3322 291.0670 16.33524131 11162

Epoch: 2024-10-06T03:48Z

Definitive object data (Epoch: 2024-10-06T03:48:10.912Z)

Latitude	23.39498°
Longitude	-75.34609°
Altitude	182.34 km
Speed	7.801 km/s
True Right ascension	23h 48m 00s
True Declination	23° 15' 32"
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	187.692 km
Perigee altitude	179.024 km
Semi-major axis	6,561.495 km
Eccentricity	0.0006605
Inclination	53.1358°
RAAN	195.8207°
Arg. of periapsis	219.3322°
True anomaly	290.99635°
Mean anomaly	291.067°
Eccentric anomaly	291.03168°
Mean motion	4.08356 °/min
BSTAR	0.0010112
Orbital period	88.16 mins