STARLINK-35040, 65480

Orbit data source: Space-Track

STARLINK-35040, 65480 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
65480, 2025-195Y
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: 12 hours ago

TLE from 12 hours ago
0 STARLINK-35040
1 65480U 25195Y   26171.32970382  .00029501  00000-0  88010-3 0  9993
2 65480  53.1581 140.3192 0001255  93.6795 266.4351 15.34425787 45709
Epoch: 2026-06-20T07:54Z
TLE epoch observation values (Epoch: 2026-06-20T07:54:46.410Z)
Latitude
-0.00001°
Longitude
113.07994°
Altitude
463.581 km
Speed
7.636 km/s
True Right ascension
09h 21m 16s
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
07:20:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.742 km
Perigee altitude
462.025 km
Semi-major axis
6,841.021 km
Eccentricity
0.00013
Inclination
53.1581°
RAAN
140.3192°
Arg. of periapsis
93.6795°
True anomaly
266.42075°
Mean anomaly
266.4351°
Eccentric anomaly
266.42792°
Mean motion
3.83585 °/min
Orbital period
93.85 mins
BSTAR
0.0008801
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
|