STARLINK-1905, 46746

Orbit data source: Space-Track

STARLINK-1905, 46746 is 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.

Loading next visibility...
Identifier
46746, 2020-074H
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
SpaceX/Seattle
Mission
Partially operational 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: 14 hours ago

TLE from 14 hours ago
0 STARLINK-1905
1 46746U 20074H   26126.02747283  .00123300  00000-0  77604-3 0  9996
2 46746  53.0405   0.3591 0005438 157.6243 202.5014 15.75826090306211
Epoch: 2026-05-06T00:39Z
TLE epoch observation values (Epoch: 2026-05-06T00:39:33.652Z)
Latitude
-0.00003°
Longitude
126.575°
Altitude
346.562 km
Speed
7.7 km/s
True Right ascension
00h 01m 26s
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
22:30:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
346.217 km
Perigee altitude
338.908 km
Semi-major axis
6,720.7 km
Eccentricity
0.00054
Inclination
53.0405°
RAAN
0.3591°
Arg. of periapsis
157.6243°
True anomaly
202.47757°
Mean anomaly
202.5014°
Eccentric anomaly
202.48948°
Mean motion
3.93932 °/min
Orbital period
91.39 mins
BSTAR
0.00077604
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|