DECAYED

STARLINK-2528, 48307 (Decayed)

Orbit data source: Space-Track

STARLINK-2528, 48307 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-2528 details

Identifier	48307, 2021-036AH
Orbit	Decayed
Last TLE update	7 months 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 7 months ago

0 STARLINK-2528
1 48307U 21036AH  24203.63775640  .08817526  12369-4  67261-3 0  9990
2 48307  53.0318 220.5882 0001956 301.0519 162.2655 16.39650971179293

Epoch: 2024-07-21T15:18Z

Definitive object data (Epoch: 2024-07-21T15:18:22.152Z)

Latitude	51.18572°
Longitude	162.63352°
Altitude	173.978 km
Speed	7.808 km/s
True Right ascension	22h 08m 25s
True Declination	51° 00' 09"
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	168.301 km
Perigee altitude	165.741 km
Semi-major axis	6,545.158 km
Eccentricity	0.0001956
Inclination	53.0318°
RAAN	220.5882°
Arg. of periapsis	301.0519°
True anomaly	162.27233°
Mean anomaly	162.2655°
Eccentric anomaly	162.26891°
Mean motion	4.09886 °/min
BSTAR	0.00067261
Orbital period	87.83 mins