OBJECT E, 68796

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 E, 68796 is a Japanese satellite in SSO that was launched on Thu, 23 Apr 2026 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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
68796, 2026-088E
Orbit
SSO
Country
Flag of JPJP / JPN
Related business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2026-04-23 (2 months ago)
Launch vehicle
ELECTRON
Launch site
Rocket Lab Launch Complex (RLLC)
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: 13 hours ago

TLE from 13 hours ago
0 OBJECT E
1 68796U 26088E   26171.41188868  .00003371  00000-0  21980-3 0  9998
2 68796  97.5072 320.7236 0017041  70.2764 290.0301 15.08450962  8788
Epoch: 2026-06-20T09:53Z
TLE epoch observation values (Epoch: 2026-06-20T09:53:07.181Z)
Latitude
-0.00005°
Longitude
-96.1832°
Altitude
539.983 km
Speed
7.595 km/s
True Right ascension
21h 22m 53s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
10:18:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
549.704 km
Perigee altitude
526.133 km
Semi-major axis
6,916.055 km
Eccentricity
0.0017
Inclination
97.5072°
RAAN
320.7236°
Arg. of periapsis
70.2764°
True anomaly
289.8465°
Mean anomaly
290.0301°
Eccentric anomaly
289.93831°
Mean motion
3.7736 °/min
Orbital period
95.4 mins
BSTAR
0.0002198
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
|