STARLINK-1653, 46352

Orbit data source: Space-Track

STARLINK-1653, 46352 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 03 Sep 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
46352, 2020-062AD
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)
2020-09-03 (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: 8 hours ago

TLE from 8 hours ago
0 STARLINK-1653
1 46352U 20062AD  26137.56638841  .00067747  00000-0  50220-3 0  9993
2 46352  53.0391 343.6995 0009396 136.1726 224.0039 15.72235830315875
Epoch: 2026-05-17T13:35Z
TLE epoch observation values (Epoch: 2026-05-17T13:35:35.958Z)
Latitude
0.00001°
Longitude
-95.46748°
Altitude
357.963 km
Speed
7.693 km/s
True Right ascension
22h 54m 47s
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
06:27:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
359.114 km
Perigee altitude
346.465 km
Semi-major axis
6,730.926 km
Eccentricity
0.00094
Inclination
53.0391°
RAAN
343.6995°
Arg. of periapsis
136.1726°
True anomaly
223.92916°
Mean anomaly
224.0039°
Eccentric anomaly
223.96653°
Mean motion
3.93035 °/min
Orbital period
91.59 mins
BSTAR
0.0005022
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|