STARLINK-1771, 46384

Orbit data source: Space-Track

STARLINK-1771, 46384 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
46384, 2020-062BM
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: 14 hours ago

TLE from 14 hours ago
0 STARLINK-1771
1 46384U 20062BM  26318.00004630  .00140003  00000-0  59037-3 0  9993
2 46384  53.0250 201.5019 0003064 134.7053 281.9964 15.84544830  5901
Epoch: 2026-11-14T00:00Z
TLE epoch observation values (Epoch: 2026-11-14T00:00:04.000Z)
Latitude
42.01017°
Longitude
-169.22579°
Altitude
321.175 km
Speed
7.721 km/s
True Right ascension
16h 15m 36s
True Declination
41° 49' 41"
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
10:41:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
319.943 km
Perigee altitude
315.84 km
Semi-major axis
6,696.028 km
Eccentricity
0.00031
Inclination
53.025°
RAAN
201.5019°
Arg. of periapsis
134.7053°
True anomaly
281.96205°
Mean anomaly
281.9964°
Eccentric anomaly
281.97923°
Mean motion
3.96111 °/min
Orbital period
90.88 mins
BSTAR
0.00059037
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|