STARLINK-1728, 46582

Orbit data source: Space-Track

STARLINK-1728, 46582 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
46582, 2020-070BC
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 (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: 9 hours ago

TLE from 9 hours ago
0 STARLINK-1728
1 46582U 20070BC  26202.33335648  .00251388  00000-0  83812-3 0  9993
2 46582  53.0276 185.6430 0007862  51.9274  20.7681 15.89005267  6012
Epoch: 2026-07-21T08:00Z
TLE epoch observation values (Epoch: 2026-07-21T08:00:01.999Z)
Latitude
49.87292°
Longitude
-170.838°
Altitude
305.91 km
Speed
7.733 km/s
True Right ascension
16h 33m 05s
True Declination
49° 41' 31"
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
06:13:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
310.61 km
Perigee altitude
300.101 km
Semi-major axis
6,683.492 km
Eccentricity
0.00079
Inclination
53.0276°
RAAN
185.643°
Arg. of periapsis
51.9274°
True anomaly
20.80007°
Mean anomaly
20.7681°
Eccentric anomaly
20.78408°
Mean motion
3.97226 °/min
Orbital period
90.63 mins
BSTAR
0.00083812
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|