DECAYED

STARLINK-2541, 48313 (Decayed)

Orbit data source: Space-Track

STARLINK-2541, 48313 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 29 Apr 2021 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-2541 details

Identifier	48313, 2021-036AP
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)	2021-04-29 (4 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-2541
1 48313U 21036AP  25007.99433022  .07830549  12178-4  13672-2 0  9997
2 48313  53.0408 182.8913 0004280 303.4676 200.6910 16.32062509204925

Epoch: 2025-01-07T23:51Z

Definitive object data (Epoch: 2025-01-07T23:51:50.131Z)

Latitude	27.99735°
Longitude	-126.29796°
Altitude	191.016 km
Speed	7.794 km/s
True Right ascension	22h 37m 49s
True Declination	27° 50' 34"
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	190.1 km
Perigee altitude	184.48 km
Semi-major axis	6,565.427 km
Eccentricity	0.000428
Inclination	53.0408°
RAAN	182.8913°
Arg. of periapsis	303.4676°
True anomaly	200.67368°
Mean anomaly	200.691°
Eccentric anomaly	200.68234°
Mean motion	4.07989 °/min
BSTAR	0.0013672
Orbital period	88.24 mins