STARLINK-1795, 46696

Orbit data source: Space-Track

STARLINK-1795, 46696 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 18 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
46696, 2020-073AC
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)
2020-10-18 (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: 18 hours ago

TLE from 18 hours ago
0 STARLINK-1795
1 46696U 20073AC  25345.12955115  .00126956  00000-0  27162-2 0  9990
2 46696  53.0537 249.0492 0011503 102.0561 258.1734 15.43828300284201
Epoch: 2025-12-11T03:06Z
TLE epoch observation values (Epoch: 2025-12-11T03:06:33.219Z)
Latitude
-0.00002°
Longitude
122.32082°
Altitude
437.331 km
Speed
7.65 km/s
True Right ascension
16h 36m 11s
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
19:37:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
442.936 km
Perigee altitude
427.261 km
Semi-major axis
6,813.235 km
Eccentricity
0.00115
Inclination
53.0537°
RAAN
249.0492°
Arg. of periapsis
102.0561°
True anomaly
258.04442°
Mean anomaly
258.1734°
Eccentric anomaly
258.10891°
Mean motion
3.85934 °/min
Orbital period
93.28 mins
BSTAR
0.0027162
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|