STARLINK-1080, 44961

Orbit data source: Space-Track

STARLINK-1080, 44961 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.

Loading next visibility...
Identifier
44961, 2020-001AZ
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, 10.1 m
Radar Cross Section
13.562 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 17 hours ago

TLE from 17 hours ago
0 STARLINK-1080
1 44961U 20001AZ  26076.81579790  .00080253  00000-0  14667-2 0  9998
2 44961  53.0490 249.3232 0005652 150.3121 209.8208 15.48693365341932
Epoch: 2026-03-17T19:34Z
TLE epoch observation values (Epoch: 2026-03-17T19:34:44.938Z)
Latitude
-0.00003°
Longitude
140.24743°
Altitude
424.777 km
Speed
7.656 km/s
True Right ascension
16h 37m 17s
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
16:54:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
424.667 km
Perigee altitude
416.981 km
Semi-major axis
6,798.961 km
Eccentricity
0.00057
Inclination
53.049°
RAAN
249.3232°
Arg. of periapsis
150.3121°
True anomaly
209.78861°
Mean anomaly
209.8208°
Eccentric anomaly
209.8047°
Mean motion
3.8715 °/min
Orbital period
92.99 mins
BSTAR
0.0014667
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|