STARLINK-1944, 46796

Orbit data source: Space-Track

STARLINK-1944, 46796 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 24 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
46796, 2020-074BK
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)
2020-10-24 (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: 8 hours ago

TLE from 8 hours ago
0 STARLINK-1944
1 46796U 20074BK  26062.66668981  .00166804  00000-0  17442-2 0  9996
2 46796  53.0467 300.4070 0000585 196.9967 225.0218 15.63420791  5843
Epoch: 2026-03-03T16:00Z
TLE epoch observation values (Epoch: 2026-03-03T16:00:01.999Z)
Latitude
45.02751°
Longitude
-52.55853°
Altitude
382.731 km
Speed
7.686 km/s
True Right ascension
23h 15m 34s
True Declination
44° 50' 46"
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
03:19:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
378.458 km
Perigee altitude
377.668 km
Semi-major axis
6,756.2 km
Eccentricity
0.00006
Inclination
53.0467°
RAAN
300.407°
Arg. of periapsis
196.9967°
True anomaly
225.01706°
Mean anomaly
225.0218°
Eccentric anomaly
225.01943°
Mean motion
3.90831 °/min
Orbital period
92.11 mins
BSTAR
0.0017442
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|