STARLINK-1096, 44942

Orbit data source: Space-Track

STARLINK-1096, 44942 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 07 Jan 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
44942, 2020-001AE
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)
2020-01-07 (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, 4.4 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-1096
1 44942U 20001AE  25260.91349994  .00084180  00000-0  55113-3 0  9998
2 44942  52.9933 164.9378 0002730 125.6331 234.4942 15.75095299317110
Epoch: 2025-09-17T21:55Z
TLE epoch observation values (Epoch: 2025-09-17T21:55:26.394Z)
Latitude
-0.00001°
Longitude
-161.00481°
Altitude
346.325 km
Speed
7.702 km/s
True Right ascension
10h 59m 45s
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
23:08:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
346.484 km
Perigee altitude
342.813 km
Semi-major axis
6,722.786 km
Eccentricity
0.00027
Inclination
52.9933°
RAAN
164.9378°
Arg. of periapsis
125.6331°
True anomaly
234.46874°
Mean anomaly
234.4942°
Eccentric anomaly
234.48147°
Mean motion
3.93749 °/min
Orbital period
91.43 mins
BSTAR
0.00055113
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|