STARLINK-30468, 57926

Orbit data source: Space-Track

STARLINK-30468, 57926 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 24 Sep 2023 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
57926, 2023-147P
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
SpaceX/Seattle
Mission
Partially operational Commercial Communications
Bus & Motor
STARLINK V2M, Unknown motor
Mass
730 kg wet, ~700 kg dry
Launch date (UTC)
2023-09-24 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 17.7 m
Radar Cross Section
33.884 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 STARLINK-30468
1 57926U 23147P   26171.17651620  .00001764  00000-0  73620-4 0  9991
2 57926  43.0022 109.6854 0001503 253.2053 106.8634 15.27583111152239
Epoch: 2026-06-20T04:14Z
TLE epoch observation values (Epoch: 2026-06-20T04:14:10.999Z)
Latitude
-0.00002°
Longitude
137.74466°
Altitude
483.115 km
Speed
7.625 km/s
True Right ascension
07h 18m 44s
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
00:39:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.016 km
Perigee altitude
483.953 km
Semi-major axis
6,863.122 km
Eccentricity
0.00015
Inclination
43.0022°
RAAN
109.6854°
Arg. of periapsis
253.2053°
True anomaly
106.87988°
Mean anomaly
106.8634°
Eccentric anomaly
106.87164°
Mean motion
3.81734 °/min
Orbital period
94.31 mins
BSTAR
0.00007362
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|