OBJECT F, 68696
Orbit data source: Space-Track
OBJECT F, 68696 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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68696 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
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 OBJECT F
1 68696U 26080F 26105.07427363 .00001014 00000-0 67432-4 0 9999
2 68696 97.6631 180.7184 0013605 281.1130 78.8569 15.09416186 104Epoch: 2026-04-15T01:46Z
TLE epoch observation values (Epoch: 2026-04-15T01:46:57.241Z)
Latitude
-0°
Longitude
-49.2615°
Altitude
539.245 km
Speed
7.594 km/s
True Right ascension
12h 02m 52s
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
03:02:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
544.379 km
Perigee altitude
525.569 km
Semi-major axis
6,913.111 km
Eccentricity
0.00136
Inclination
97.6631°
RAAN
180.7184°
Arg. of periapsis
281.113°
True anomaly
79.00991°
Mean anomaly
78.8569°
Eccentric anomaly
78.9334°
Mean motion
3.77601 °/min
Orbital period
95.34 mins
BSTAR
0.000067432
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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 F 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 | 2026-04-16 04:56:54.167Z | 162.775° S | 2026-04-16 05:00:54.167Z | 14.34° NNE | 43.126° | 2026-04-16 05:03:54.167Z | 350.491° N |
| 6 mins | 2026-04-16 18:07:54.167Z | 359.054° N | 2026-04-16 18:09:54.167Z | 319.118° NNW | 39.005° | 2026-04-16 18:13:54.167Z | 206.604° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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