STARLINK-1677, 46576

Orbit data source: Space-Track

STARLINK-1677, 46576 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
46576, 2020-070AW
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: 6 hours ago

TLE from 6 hours ago
0 STARLINK-1677
1 46576U 20070AW  25337.91484065  .00123852  00000-0  32818-2 0  9999
2 46576  53.0484 223.0500 0009481 113.1193 247.0809 15.37394054285407
Epoch: 2025-12-03T21:57Z
TLE epoch observation values (Epoch: 2025-12-03T21:57:22.232Z)
Latitude
-0.00005°
Longitude
-179.27146°
Altitude
457.237 km
Speed
7.638 km/s
True Right ascension
14h 52m 11s
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
02:14:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
460.572 km
Perigee altitude
447.616 km
Semi-major axis
6,832.231 km
Eccentricity
0.00095
Inclination
53.0484°
RAAN
223.05°
Arg. of periapsis
113.1193°
True anomaly
246.98088°
Mean anomaly
247.0809°
Eccentric anomaly
247.03088°
Mean motion
3.84326 °/min
Orbital period
93.67 mins
BSTAR
0.0032818
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|