STARLINK-31312, 59152

Orbit data source: Space-Track

STARLINK-31312, 59152 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 04 Mar 2024 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
59152, 2024-044A
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2M, Unknown motor
Mass
730 kg wet, ~700 kg dry
Launch date (UTC)
2024-03-04 (2 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, 14.5 m
Radar Cross Section
33.884 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 STARLINK-31312
1 59152U 24044A   25251.01931202  .00000310  00000-0  20784-4 0  9998
2 59152  43.0014   7.9476 0001132 286.5427  73.5300 15.27564698 86241
Epoch: 2025-09-08T00:27Z
TLE epoch observation values (Epoch: 2025-09-08T00:27:48.558Z)
Latitude
-0.00004°
Longitude
13.66479°
Altitude
482.65 km
Speed
7.626 km/s
True Right ascension
00h 31m 47s
True Declination
0° 00' 00"
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
06:21:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.817 km
Perigee altitude
484.263 km
Semi-major axis
6,863.177 km
Eccentricity
0.00011
Inclination
43.0014°
RAAN
7.9476°
Arg. of periapsis
286.5427°
True anomaly
73.54244°
Mean anomaly
73.53°
Eccentric anomaly
73.53622°
Mean motion
3.81729 °/min
Orbital period
94.31 mins
BSTAR
0.000020784
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
|