STARLINK-1928, 46758

Orbit data source: Space-Track

STARLINK-1928, 46758 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 24 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
46758, 2020-074V
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)
2020-10-24 (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-1928
1 46758U 20074V   26173.00637890  .01434861  11797-4  75099-3 0  9994
2 46758  53.0260 119.4661 0005358 229.8200 130.2369 16.19491051313716
Epoch: 2026-06-22T00:09Z
TLE epoch observation values (Epoch: 2026-06-22T00:09:11.136Z)
Latitude
-0.00004°
Longitude
-153.02882°
Altitude
224.138 km
Speed
7.772 km/s
True Right ascension
07h 57m 51s
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
21:36:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
224.758 km
Perigee altitude
217.687 km
Semi-major axis
6,599.36 km
Eccentricity
0.00054
Inclination
53.026°
RAAN
119.4661°
Arg. of periapsis
229.82°
True anomaly
130.28375°
Mean anomaly
130.2369°
Eccentric anomaly
130.26033°
Mean motion
4.04847 °/min
Orbital period
88.92 mins
BSTAR
0.00075099
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Computing Atmospheric mass density...

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