DECAYED

STARLINK-32187, 60337 (Decayed)

Orbit data source: Space-Track

STARLINK-32187, 60337 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Fri, 02 Aug 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-32187 details

Identifier	60337, 2024-136J
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)	2024-08-02 (5 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-32187
1 60337U 24136J   24269.17904794  .04247004  12144-4  84954-3 0  9999
2 60337  53.1356   9.1664 0010681 345.3007  93.1598 16.30510420  9701

Epoch: 2024-09-25T04:17Z

Definitive object data (Epoch: 2024-09-25T04:17:49.742Z)

Latitude	51.80588°
Longitude	11.60112°
Altitude	197.746 km
Speed	7.794 km/s
True Right ascension	05h 22m 09s
True Declination	51° 37' 28"
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	198.457 km
Perigee altitude	184.423 km
Semi-major axis	6,569.577 km
Eccentricity	0.0010681
Inclination	53.1356°
RAAN	9.1664°
Arg. of periapsis	345.3007°
True anomaly	93.282°
Mean anomaly	93.1598°
Eccentric anomaly	93.2209°
Mean motion	4.07603 °/min
BSTAR	0.00084954
Orbital period	88.32 mins