STARLINK-1680, 46558

Orbit data source: Space-Track

STARLINK-1680, 46558 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
46558, 2020-070AC
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: 10 hours ago

TLE from 10 hours ago
0 STARLINK-1680
1 46558U 20070AC  26019.33335648  .00266777  00000-0  33920-2 0  9994
2 46558  53.0493 352.6232 0003375  33.0903 216.5514 15.57962178  5788
Epoch: 2026-01-19T08:00Z
TLE epoch observation values (Epoch: 2026-01-19T08:00:01.999Z)
Latitude
-48.6928°
Longitude
-7.77043°
Altitude
412.097 km
Speed
7.662 km/s
True Right ascension
15h 23m 52s
True Declination
-48° 30' 49"
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
18:56:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
396.119 km
Perigee altitude
391.548 km
Semi-major axis
6,771.97 km
Eccentricity
0.00034
Inclination
53.0493°
RAAN
352.6232°
Arg. of periapsis
33.0903°
True anomaly
216.52838°
Mean anomaly
216.5514°
Eccentric anomaly
216.53989°
Mean motion
3.89467 °/min
Orbital period
92.43 mins
BSTAR
0.003392
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|