OBJECT L, 68426

Orbit data source: Space-Track

You're viewing an uncataloged RSO

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 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). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity.

Loading next visibility...
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 (5 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Unknown
Shape & HBR
Box, 1.1 m
Radar Cross Section
0.015 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 17 hours ago

TLE from 17 hours ago
0 OBJECT L
1 68426U 26067L   26228.38452834  .00007283  00000-0  33271-3 0  9993
2 68426  97.4592 186.2894 0003707 105.5418 254.6227 15.20867863 21099
Epoch: 2026-08-16T09:13Z
TLE epoch observation values (Epoch: 2026-08-16T09:13:43.248Z)
Latitude
-0.00002°
Longitude
83.07738°
Altitude
506.989 km
Speed
7.61 km/s
True Right ascension
12h 25m 09s
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
16:37:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.738 km
Perigee altitude
497.639 km
Semi-major axis
6,878.325 km
Eccentricity
0.00037
Inclination
97.4592°
RAAN
186.2894°
Arg. of periapsis
105.5418°
True anomaly
254.58175°
Mean anomaly
254.6227°
Eccentric anomaly
254.60222°
Mean motion
3.80469 °/min
Orbital period
94.62 mins
BSTAR
0.00033271
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
|