OBJECT E, 68695
Orbit data source: Space-Track
OBJECT E, 68695 is a satellite owned by Changguang WJ (CN) in SSO that was launched on Tue, 14 Apr 2026 UTC via a LIJIAN-1 launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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.
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68695 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Changguang WJ
Mission
Operational spacecraft
Bus & Motor
JL-1GF07, Unknown motor
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 OBJECT E
1 68695U 26080E 26138.81473466 .00004202 00000-0 26411-3 0 9994
2 68695 97.6646 214.4509 0016794 158.4624 201.7315 15.09684131 5198Epoch: 2026-05-18T19:33Z
TLE epoch observation values (Epoch: 2026-05-18T19:33:13.074Z)
Latitude
-0.00002°
Longitude
44.64884°
Altitude
551.026 km
Speed
7.58 km/s
True Right ascension
14h 17m 48s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
10:11:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
545.764 km
Perigee altitude
522.547 km
Semi-major axis
6,912.292 km
Eccentricity
0.00168
Inclination
97.6646°
RAAN
214.4509°
Arg. of periapsis
158.4624°
True anomaly
201.66038°
Mean anomaly
201.7315°
Eccentric anomaly
201.69593°
Mean motion
3.77668 °/min
Orbital period
95.32 mins
BSTAR
0.00026411
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Other satellites on launch #80 in the year 2026 (2026-04-14 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.OBJECT E Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-19 05:13:02.620Z | 176.332° S | 2026-05-19 05:16:02.620Z | 218.117° SW | 41.13° | 2026-05-19 05:20:02.620Z | 341.585° N |
| 5 mins | 2026-05-19 18:24:02.620Z | 342.991° N | 2026-05-19 18:26:02.620Z | 287.697° WNW | 31.809° | 2026-05-19 18:29:02.620Z | 221.981° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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