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OBJECT L, 68426

Orbit data source: Space-Track

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Recently launched and/or uncataloged RSOs may have evolving metadata. Metadata may include the following, but is not limited to: Owner, Manufacturer, Bus, Motor, and Mission.

OBJECT L, 68426 is a payload satellite in SSO that was launched on Mon, 30 Mar 2026 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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.

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Identifier
68426, 2026-067L
Orbit
SSO
Country
Flag of TBDTBD
Related business
Manufacturer
Endurosat
Mission
Operational Civil Technology
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
2026-03-30 (7 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.087 m
Radar Cross Section
0.015 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 21 hours ago

TLE from 21 hours ago
0 OBJECT L
1 68426U 26067L   26307.88231281  .00011188  00000-0  48092-3 0  9993
2 68426  97.4723 265.1755 0002208 118.0533 242.0927 15.22826333 33180
Epoch: 2026-11-03T21:10Z
TLE epoch observation values (Epoch: 2026-11-03T21:10:31.826Z)
Latitude
-0.00004°
Longitude
-95.59571°
Altitude
501.124 km
Speed
7.613 km/s
True Right ascension
17h 40m 42s
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
14:34:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.803 km
Perigee altitude
492.768 km
Semi-major axis
6,872.422 km
Eccentricity
0.00022
Inclination
97.4723°
RAAN
265.1755°
Arg. of periapsis
118.0533°
True anomaly
242.07034°
Mean anomaly
242.0927°
Eccentric anomaly
242.08152°
Mean motion
3.80959 °/min
Orbital period
94.5 mins
BSTAR
0.00048092
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