DECAYED

STARLINK-1793, 46694 (Decayed)

Orbit data source: Space-Track

STARLINK-1793, 46694 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 18 Oct 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
46694, 2020-073AA
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)
2020-10-18 (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: 6 months ago

TLE from 6 months ago
0 STARLINK-1793
1 46694U 20073AA  25110.10965370  .12231848  12506-4  71431-3 0  9997
2 46694  53.0355 198.6979 0006704 329.5612 103.4224 16.41689244249620
Epoch: 2025-04-20T02:37Z
TLE epoch observation values (Epoch: 2025-04-20T02:37:54.079Z)
Latitude
50.00334°
Longitude
13.88438°
Altitude
168.093 km
Speed
7.811 km/s
True Right ascension
17h 27m 12s
True Declination
49° 49' 07"
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
02:26:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
165.986 km
Perigee altitude
157.218 km
Semi-major axis
6,539.739 km
Eccentricity
0.00067
Inclination
53.0355°
RAAN
198.6979°
Arg. of periapsis
329.5612°
True anomaly
103.49711°
Mean anomaly
103.4224°
Eccentric anomaly
103.45976°
Mean motion
4.10395 °/min
Orbital period
87.72 mins
BSTAR
0.00071431
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|