STARLINK-34031, 63912

Orbit data source: Space-Track

STARLINK-34031, 63912 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 10 May 2025 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
63912, 2025-095Y
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
2025-05-10 (1 year 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
36.964 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 STARLINK-34031
1 63912U 25095Y   26171.45590764  .00017745  00000-0  65247-3 0  9990
2 63912  43.0033 315.9267 0002417 271.8494  88.2081 15.27595800 63499
Epoch: 2026-06-20T10:56Z
TLE epoch observation values (Epoch: 2026-06-20T10:56:30.420Z)
Latitude
0.00001°
Longitude
-116.87032°
Altitude
482.726 km
Speed
7.626 km/s
True Right ascension
21h 03m 42s
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
09:53:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.605 km
Perigee altitude
483.288 km
Semi-major axis
6,863.083 km
Eccentricity
0.00024
Inclination
43.0033°
RAAN
315.9267°
Arg. of periapsis
271.8494°
True anomaly
88.23578°
Mean anomaly
88.2081°
Eccentric anomaly
88.22194°
Mean motion
3.81737 °/min
Orbital period
94.31 mins
BSTAR
0.00065247
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
|