DECAYED

STARLINK-1624, 46130 (Decayed)

Orbit data source: Space-Track

STARLINK-1624, 46130 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 18 Aug 2020 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
46130, 2020-057P
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)
2020-08-18 (6 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: 4 weeks ago

TLE from 4 weeks ago
0 STARLINK-1624
1 46130U 20057P   26147.01126124  .11295235  12524-4  45513-3 0  9992
2 46130  53.0127 195.9911 0005715 310.4290  49.6259 16.43550406320921
Epoch: 2026-05-27T00:16Z
TLE epoch observation values (Epoch: 2026-05-27T00:16:12.971Z)
Latitude
0.00003°
Longitude
-52.6394°
Altitude
154.884 km
Speed
7.816 km/s
True Right ascension
13h 03m 57s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
23:19:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
160.403 km
Perigee altitude
152.934 km
Semi-major axis
6,534.805 km
Eccentricity
0.00057
Inclination
53.0127°
RAAN
195.9911°
Arg. of periapsis
310.429°
True anomaly
49.67581°
Mean anomaly
49.6259°
Eccentric anomaly
49.65086°
Mean motion
4.1086 °/min
Orbital period
87.62 mins
BSTAR
0.00045513
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|