STARLINK-31286, 59082

Orbit data source: Space-Track

STARLINK-31286, 59082 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 29 Feb 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
59082, 2024-041J
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)
2024-02-29 (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, 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-31286
1 59082U 24041J   26171.14804328 -.00000786  00000-0 -19017-4 0  9997
2 59082  42.9996  91.8685 0001862 258.8116 101.2527 15.27587659130029
Epoch: 2026-06-20T03:33Z
TLE epoch observation values (Epoch: 2026-06-20T03:33:10.939Z)
Latitude
0.00003°
Longitude
130.20612°
Altitude
483.051 km
Speed
7.626 km/s
True Right ascension
06h 07m 28s
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
21:26:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.249 km
Perigee altitude
483.693 km
Semi-major axis
6,863.108 km
Eccentricity
0.00019
Inclination
42.9996°
RAAN
91.8685°
Arg. of periapsis
258.8116°
True anomaly
101.27363°
Mean anomaly
101.2527°
Eccentric anomaly
101.26316°
Mean motion
3.81735 °/min
Orbital period
94.31 mins
BSTAR
-0.000019017
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
|