STARLINK-1686, 46328

Orbit data source: Space-Track

STARLINK-1686, 46328 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 03 Sep 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
46328, 2020-062D
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)
2020-09-03 (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-1686
1 46328U 20062D   25335.00002315  .00084959  00000-0  20405-2 0  9990
2 46328  53.0509  70.9074 0005769 314.3954 235.8591 15.40627379  5888
Epoch: 2025-12-01T00:00Z
TLE epoch observation values (Epoch: 2025-12-01T00:00:02.000Z)
Latitude
-8.26423°
Longitude
-172.96966°
Altitude
448.8 km
Speed
7.642 km/s
True Right ascension
17h 08m 34s
True Declination
-8° 12' 48"
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
07:56:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
448.468 km
Perigee altitude
440.596 km
Semi-major axis
6,822.669 km
Eccentricity
0.00058
Inclination
53.0509°
RAAN
70.9074°
Arg. of periapsis
314.3954°
True anomaly
235.80441°
Mean anomaly
235.8591°
Eccentric anomaly
235.83175°
Mean motion
3.85134 °/min
Orbital period
93.47 mins
BSTAR
0.0020405
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
|