DECAYED

STARLINK-1618, 46125 (Decayed)

Orbit data source: Space-Track

STARLINK-1618, 46125 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
46125, 2020-057J
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: 6 months ago

TLE from 6 months ago
0 STARLINK-1618
1 46125U 20057J   25260.04934914  .08411337  12364-4  84879-3 0  9997
2 46125  53.0242 319.4367 0005174 335.2533  24.8263 16.37211303281946
Epoch: 2025-09-17T01:11Z
TLE epoch observation values (Epoch: 2025-09-17T01:11:03.765Z)
Latitude
-0.00004°
Longitude
-54.5599°
Altitude
171.081 km
Speed
7.807 km/s
True Right ascension
21h 17m 44s
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
07:09:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
176.912 km
Perigee altitude
170.132 km
Semi-major axis
6,551.659 km
Eccentricity
0.00052
Inclination
53.0242°
RAAN
319.4367°
Arg. of periapsis
335.2533°
True anomaly
24.85121°
Mean anomaly
24.8263°
Eccentric anomaly
24.83875°
Mean motion
4.09276 °/min
Orbital period
87.96 mins
BSTAR
0.00084879
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|