STARLINK-1746, 46588

Orbit data source: Space-Track

STARLINK-1746, 46588 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 06 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
46588, 2020-070BJ
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)
2020-10-06 (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: 19 hours ago

TLE from 19 hours ago
0 STARLINK-1746
1 46588U 20070BJ  25333.15455105  .00084642  00000-0  21093-2 0  9993
2 46588  53.0533 240.2742 0008479 104.0814 256.1132 15.39490247284748
Epoch: 2025-11-29T03:42Z
TLE epoch observation values (Epoch: 2025-11-29T03:42:33.210Z)
Latitude
-0.00006°
Longitude
116.34895°
Altitude
449.901 km
Speed
7.643 km/s
True Right ascension
16h 01m 05s
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
20:45:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
453.678 km
Perigee altitude
442.103 km
Semi-major axis
6,826.027 km
Eccentricity
0.00085
Inclination
53.0533°
RAAN
240.2742°
Arg. of periapsis
104.0814°
True anomaly
256.0189°
Mean anomaly
256.1132°
Eccentric anomaly
256.06605°
Mean motion
3.8485 °/min
Orbital period
93.54 mins
BSTAR
0.0021093
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|