OBJECT L, 68426

Orbit data source: Space-Track

You're viewing an Uncataloged Satellite

Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, 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 spacecraft
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
2026-03-30 (3 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Unknown
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 OBJECT L
1 68426U 26067L   26170.86156886  .00009224  00000-0  43387-3 0  9996
2 68426  97.4544 129.3983 0002115  50.2549 309.8872 15.19786006 12351
Epoch: 2026-06-19T20:40Z
TLE epoch observation values (Epoch: 2026-06-19T20:40:39.549Z)
Latitude
-0.00002°
Longitude
-88.85095°
Altitude
508.642 km
Speed
7.61 km/s
True Right ascension
08h 37m 35s
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
07:13:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.91 km
Perigee altitude
502 km
Semi-major axis
6,881.592 km
Eccentricity
0.00021
Inclination
97.4544°
RAAN
129.3983°
Arg. of periapsis
50.2549°
True anomaly
309.8686°
Mean anomaly
309.8872°
Eccentric anomaly
309.8779°
Mean motion
3.80198 °/min
Orbital period
94.69 mins
BSTAR
0.00043387
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
|