OBJECT A, 100651
Orbit data source: Space-Track
OBJECT A, 100651 is a satellite owned by PLA SSF (CN) in LEO that was launched on Thu, 10 Sep 2026 UTC launched 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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100651 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
DFH
Mission
Operational spacecraft
Bus & Motor
YG53, Unknown motor
Mass
~250 kg wet, ~250 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Unknown
Shape & HBR
BOX + 2 PAN, 2.5 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 OBJECT A
1 A0651U 26205A 26258.49929604 -.00010485 00000-0 -52922-3 0 9996
2 A0651 45.0095 80.8068 0006132 295.7243 64.3003 15.15632017 783Epoch: 2026-09-15T11:58Z
TLE epoch observation values (Epoch: 2026-09-15T11:58:59.177Z)
Latitude
0.00002°
Longitude
-93.40412°
Altitude
517.228 km
Speed
7.608 km/s
True Right ascension
05h 23m 13s
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
02:02:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
524.89 km
Perigee altitude
516.429 km
Semi-major axis
6,898.797 km
Eccentricity
0.00061
Inclination
45.0095°
RAAN
80.8068°
Arg. of periapsis
295.7243°
True anomaly
64.36364°
Mean anomaly
64.3003°
Eccentric anomaly
64.33197°
Mean motion
3.78777 °/min
Orbital period
95.04 mins
BSTAR
-0.00052922
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Other satellites on launch #205 in the year 2026 (2026-09-10 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 A 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 | 2026-09-17 14:48:01.954Z | 218.92° SW | 2026-09-17 14:51:01.954Z | 156.22° SSE | 46.395° | 2026-09-17 14:55:01.954Z | 74.413° E |
| 6 mins | 2026-09-17 16:28:01.954Z | 273.435° WNW | 2026-09-17 16:31:01.954Z | 359.35° N | 50.662° | 2026-09-17 16:34:01.954Z | 59.904° ENE |
| 5 mins | 2026-09-17 18:09:01.954Z | 311.417° NW | 2026-09-17 18:11:01.954Z | 10.978° NNE | 38.947° | 2026-09-17 18:14:01.954Z | 70.951° E |
| 6 mins | 2026-09-17 19:48:01.954Z | 296.507° NW | 2026-09-17 19:51:01.954Z | 70.142° E | 74.972° | 2026-09-17 19:54:01.954Z | 109.203° ESE |
| 5 mins | 2026-09-17 21:28:01.954Z | 259.368° W | 2026-09-17 21:30:01.954Z | 220.049° SW | 23.271° | 2026-09-17 21:33:01.954Z | 167.399° S |
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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