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

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 OBJECT L
1 68426U 26067L   26257.85451354  .00011701  00000-0  52342-3 0  9993
2 68426  97.4640 215.4890 0003371  64.9030 295.2555 15.21450456 25578
Epoch: 2026-09-14T20:30Z
TLE epoch observation values (Epoch: 2026-09-14T20:30:29.969Z)
Latitude
-0.00007°
Longitude
-85.9647°
Altitude
503.566 km
Speed
7.613 km/s
True Right ascension
14h 21m 57s
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
03:00:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.749 km
Perigee altitude
496.113 km
Semi-major axis
6,876.568 km
Eccentricity
0.00034
Inclination
97.464°
RAAN
215.489°
Arg. of periapsis
64.903°
True anomaly
295.22056°
Mean anomaly
295.2555°
Eccentric anomaly
295.23803°
Mean motion
3.80615 °/min
Orbital period
94.58 mins
BSTAR
0.00052342
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
|