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). Payload-class satellites include a variety of spacecraft 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
Identifier
48313, 2021-036AP
Orbit
Decayed
Country
Flag of USUS
Related business
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 (5 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, 10.1 m
Radar Cross Section
13.562 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 11 months ago

TLE from 11 months 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
TLE epoch observation values (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 epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
06:26:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
190.1 km
Perigee altitude
184.48 km
Semi-major axis
6,565.427 km
Eccentricity
0.00043
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
Orbital period
88.24 mins
BSTAR
0.0013672
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|