OBJECT F, 68203
Orbit data source: Space-Track
OBJECT F, 68203 is a Chinese satellite in SSO that was launched on Mon, 16 Mar 2026 UTC via a KUAIZHOU-11 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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68203 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
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: 6 hours ago
TLE from 6 hours ago
0 OBJECT F
1 68203U 26052F 26077.60255771 .00005296 00000-0 32481-3 0 9992
2 68203 97.5384 153.8218 0009387 253.3003 106.7196 15.10527017 377Epoch: 2026-03-18T14:27Z
TLE epoch observation values (Epoch: 2026-03-18T14:27:40.986Z)
Latitude
-0.00006°
Longitude
120.73706°
Altitude
539.538 km
Speed
7.592 km/s
True Right ascension
10h 15m 17s
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
00:45:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
538.062 km
Perigee altitude
525.09 km
Semi-major axis
6,909.713 km
Eccentricity
0.00094
Inclination
97.5384°
RAAN
153.8218°
Arg. of periapsis
253.3003°
True anomaly
106.82258°
Mean anomaly
106.7196°
Eccentric anomaly
106.7711°
Mean motion
3.77879 °/min
Orbital period
95.27 mins
BSTAR
0.00032481
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Other satellites on launch #52 in the year 2026 (2026-03-16 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-03-19 04:54:07.229Z | 156.944° SSE | 2026-03-19 04:57:07.229Z | 57.199° ENE | 42.954° | 2026-03-19 05:00:07.229Z | 354.205° N |
| 5 mins | 2026-03-19 18:04:07.229Z | 1.115° NNE | 2026-03-19 18:06:07.229Z | 298.175° NW | 42.577° | 2026-03-19 18:09:07.229Z | 204.086° 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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