DECAYED

STARLINK-1905, 46746 (Decayed)

Orbit data source: Space-Track

STARLINK-1905, 46746 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 24 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
46746, 2020-074H
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)
2020-10-24 (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: 1 month ago

TLE from 1 month ago
0 STARLINK-1905
1 46746U 20074H   26186.91103163  .10668105  12438-4  32174-3 0  9996
2 46746  53.0199  49.8931 0010173 255.1698 104.8223 16.44282955315902
Epoch: 2026-07-05T21:51Z
TLE epoch observation values (Epoch: 2026-07-05T21:51:53.132Z)
Latitude
-0.00007°
Longitude
158.01809°
Altitude
157.068 km
Speed
7.812 km/s
True Right ascension
03h 19m 34s
True Declination
0° 00' 00"
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
15:06:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
161.372 km
Perigee altitude
148.08 km
Semi-major axis
6,532.863 km
Eccentricity
0.00102
Inclination
53.0199°
RAAN
49.8931°
Arg. of periapsis
255.1698°
True anomaly
104.93496°
Mean anomaly
104.8223°
Eccentric anomaly
104.87863°
Mean motion
4.11044 °/min
Orbital period
87.58 mins
BSTAR
0.00032174
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|