STARLINK-1678, 46538

Orbit data source: Space-Track

STARLINK-1678, 46538 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.

Not visible in the next 10 days
Identifier
46538, 2020-070G
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: 10 hours ago

TLE from 10 hours ago
0 STARLINK-1678
1 46538U 20070G   26169.33335648  .00311890  47523-4  95518-3 0  9992
2 46538  53.0306 330.3165 0005472 273.2431  80.4476 15.91406040  5965
Epoch: 2026-06-18T08:00Z
TLE epoch observation values (Epoch: 2026-06-18T08:00:01.999Z)
Latitude
-5.10104°
Longitude
-60.10091°
Altitude
299.455 km
Speed
7.729 km/s
True Right ascension
21h 45m 56s
True Declination
-5° 04' 07"
Sunlit
Object was in full shadow 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
05:04:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
302.285 km
Perigee altitude
294.978 km
Semi-major axis
6,676.769 km
Eccentricity
0.00055
Inclination
53.0306°
RAAN
330.3165°
Arg. of periapsis
273.2431°
True anomaly
80.50944°
Mean anomaly
80.4476°
Eccentric anomaly
80.47852°
Mean motion
3.97826 °/min
Orbital period
90.49 mins
BSTAR
0.00095518
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|