STARLINK-1714, 46562

Orbit data source: Space-Track

STARLINK-1714, 46562 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 06 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
46562, 2020-070AG
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)
2020-10-06 (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: 5 hours ago

TLE from 5 hours ago
0 STARLINK-1714
1 46562U 20070AG  26019.33335648  .00186158  00000-0  42786-2 0  9993
2 46562  53.0507 351.5519 0008938  50.4439 305.8723 15.41457652  5831
Epoch: 2026-01-19T08:00Z
TLE epoch observation values (Epoch: 2026-01-19T08:00:01.999Z)
Latitude
-3.10873°
Longitude
110.48427°
Altitude
439.587 km
Speed
7.651 km/s
True Right ascension
23h 16m 53s
True Declination
-3° 05' 21"
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
13:40:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
448.178 km
Perigee altitude
435.986 km
Semi-major axis
6,820.219 km
Eccentricity
0.00089
Inclination
53.0507°
RAAN
351.5519°
Arg. of periapsis
50.4439°
True anomaly
305.78925°
Mean anomaly
305.8723°
Eccentric anomaly
305.83078°
Mean motion
3.85341 °/min
Orbital period
93.42 mins
BSTAR
0.0042786
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|