STARLINK-1716, 46672

Orbit data source: Space-Track

STARLINK-1716, 46672 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 18 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
46672, 2020-073C
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)
2020-10-18 (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: 5 hours ago

TLE from 5 hours ago
0 STARLINK-1716
1 46672U 20073C   26119.33335648  .00099073  00000-0  62365-3 0  9994
2 46672  53.0402 310.7065 0005384 173.7140  98.6337 15.75917188  5931
Epoch: 2026-04-29T08:00Z
TLE epoch observation values (Epoch: 2026-04-29T08:00:01.999Z)
Latitude
-53.12813°
Longitude
-112.60538°
Altitude
361.005 km
Speed
7.692 km/s
True Right ascension
14h 58m 47s
True Declination
-52° 57' 11"
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
20:06:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
345.922 km
Perigee altitude
338.685 km
Semi-major axis
6,720.441 km
Eccentricity
0.00054
Inclination
53.0402°
RAAN
310.7065°
Arg. of periapsis
173.714°
True anomaly
98.69469°
Mean anomaly
98.6337°
Eccentric anomaly
98.6642°
Mean motion
3.93955 °/min
Orbital period
91.38 mins
BSTAR
0.00062365
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|