STARLINK-35042, 65481

Orbit data source: Space-Track

STARLINK-35042, 65481 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 03 Sep 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
65481, 2025-195Z
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)
2025-09-03 (10 months 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: 15 hours ago

TLE from 15 hours ago
0 STARLINK-35042
1 65481U 25195Z   26171.34233523  .00020314  00000-0  61054-3 0  9997
2 65481  53.1583 140.4209 0000839  50.9427 309.1650 15.34409346 45707
Epoch: 2026-06-20T08:12Z
TLE epoch observation values (Epoch: 2026-06-20T08:12:57.763Z)
Latitude
-0.00005°
Longitude
108.62185°
Altitude
463.214 km
Speed
7.636 km/s
True Right ascension
09h 21m 41s
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
10:17:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.507 km
Perigee altitude
462.359 km
Semi-major axis
6,841.07 km
Eccentricity
0.00008
Inclination
53.1583°
RAAN
140.4209°
Arg. of periapsis
50.9427°
True anomaly
309.15755°
Mean anomaly
309.165°
Eccentric anomaly
309.16127°
Mean motion
3.83581 °/min
Orbital period
93.85 mins
BSTAR
0.00061054
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
|