STARLINK-1545, 46156

Orbit data source: Space-Track

STARLINK-1545, 46156 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 18 Aug 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.

Not visible in the next 10 days
Identifier
46156, 2020-057AR
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)
2020-08-18 (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: 2 days ago

TLE from 2 days ago
0 STARLINK-1545
1 46156U 20057AR  26171.50003471  .00281277  41009-4  81861-3 0  9995
2 46156  53.0347 107.1300 0003340 204.4066 242.4347 15.92426701  6009
Epoch: 2026-06-20T12:00Z
TLE epoch observation values (Epoch: 2026-06-20T12:00:02.998Z)
Latitude
53.07259°
Longitude
103.0979°
Altitude
303.002 km
Speed
7.732 km/s
True Right ascension
12h 47m 17s
True Declination
52° 53' 46"
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
21:40:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
298.007 km
Perigee altitude
293.549 km
Semi-major axis
6,673.915 km
Eccentricity
0.00033
Inclination
53.0347°
RAAN
107.13°
Arg. of periapsis
204.4066°
True anomaly
242.40078°
Mean anomaly
242.4347°
Eccentric anomaly
242.41774°
Mean motion
3.98082 °/min
Orbital period
90.43 mins
BSTAR
0.00081861
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|