STARLINK-1042, 44747

Orbit data source: Space-Track

STARLINK-1042, 44747 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 11 Nov 2019 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
44747, 2019-074AL
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)
2019-11-11 (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: 18 hours ago

TLE from 18 hours ago
0 STARLINK-1042
1 44747U 19074AL  25241.18126517  .00017024  00000-0  42858-3 0  9996
2 44747  53.0482 291.4177 0002036 316.2245  43.8597 15.40045562320312
Epoch: 2025-08-29T04:21Z
TLE epoch observation values (Epoch: 2025-08-29T04:21:01.31Z)
Latitude
-0.00003°
Longitude
-111.47138°
Altitude
445.865 km
Speed
7.646 km/s
True Right ascension
19h 25m 40s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
14:00:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
447.64 km
Perigee altitude
444.861 km
Semi-major axis
6,824.387 km
Eccentricity
0.0002
Inclination
53.0482°
RAAN
291.4177°
Arg. of periapsis
316.2245°
True anomaly
43.87587°
Mean anomaly
43.8597°
Eccentric anomaly
43.86778°
Mean motion
3.84988 °/min
Orbital period
93.51 mins
BSTAR
0.00042858
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|