STARLINK-36324, 68091

Orbit data source: Space-Track

STARLINK-36324, 68091 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 04 Mar 2026 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
68091, 2026-042Y
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)
2026-03-04 (4 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: 11 hours ago

TLE from 11 hours ago
0 STARLINK-36324
1 68091U 26042Y   26171.39109481  .00026967  00000-0  80600-3 0  9997
2 68091  53.1584  59.9484 0001612  66.6276 293.4896 15.34415622 18052
Epoch: 2026-06-20T09:23Z
TLE epoch observation values (Epoch: 2026-06-20T09:23:10.591Z)
Latitude
-0.00003°
Longitude
10.54786°
Altitude
463.119 km
Speed
7.636 km/s
True Right ascension
03h 59m 47s
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
07:18:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.017 km
Perigee altitude
461.811 km
Semi-major axis
6,841.051 km
Eccentricity
0.00016
Inclination
53.1584°
RAAN
59.9484°
Arg. of periapsis
66.6276°
True anomaly
293.47266°
Mean anomaly
293.4896°
Eccentric anomaly
293.48113°
Mean motion
3.83583 °/min
Orbital period
93.85 mins
BSTAR
0.000806
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
|