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.

Not visible in the next 10 days
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 (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: 4 hours ago

TLE from 4 hours ago
0 STARLINK-1746
1 46588U 20070BJ  26123.33334491  .00466527  10294-3  96886-3 0  9993
2 46588  53.0293 199.5336 0012834 351.2934 204.8595 15.98424682  6026
Epoch: 2026-05-03T08:00Z
TLE epoch observation values (Epoch: 2026-05-03T08:00:01.000Z)
Latitude
-12.9499°
Longitude
48.20175°
Altitude
290.022 km
Speed
7.73 km/s
True Right ascension
01h 57m 46s
True Declination
-12° 52' 11"
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
19:52:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
287.618 km
Perigee altitude
270.531 km
Semi-major axis
6,657.211 km
Eccentricity
0.00128
Inclination
53.0293°
RAAN
199.5336°
Arg. of periapsis
351.2934°
True anomaly
204.79776°
Mean anomaly
204.8595°
Eccentric anomaly
204.82862°
Mean motion
3.99581 °/min
Orbital period
90.09 mins
BSTAR
0.00096886
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|