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.

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

TLE from 9 hours ago
0 STARLINK-1686
1 46328U 20062D   26111.00002315  .00184224  00000-0  79587-3 0  9995
2 46328  53.0365 103.1283 0011424  64.6197 126.7486 15.83817708  6008
Epoch: 2026-04-21T00:00Z
TLE epoch observation values (Epoch: 2026-04-21T00:00:02.000Z)
Latitude
-9.28128°
Longitude
81.06216°
Altitude
326.813 km
Speed
7.71 km/s
True Right ascension
19h 20m 36s
True Declination
-9° 13' 23"
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
16:14:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
327.59 km
Perigee altitude
312.287 km
Semi-major axis
6,698.075 km
Eccentricity
0.00114
Inclination
53.0365°
RAAN
103.1283°
Arg. of periapsis
64.6197°
True anomaly
126.8534°
Mean anomaly
126.7486°
Eccentric anomaly
126.80101°
Mean motion
3.9593 °/min
Orbital period
90.93 mins
BSTAR
0.00079587
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|