OBJECT A, 100780
Orbit data source: Space-Track
OBJECT A, 100780 is a Chinese satellite in SSO that was launched on Mon, 21 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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100780 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
Unknown
Launch site
Object type
Unknown
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 OBJECT A
1 A0780U 26220A 26264.53752838 .00002808 00000-0 17360-3 0 9996
2 A0780 97.5465 337.9899 0013505 271.9932 87.9751 15.10597013 210Epoch: 2026-09-21T12:54Z
TLE epoch observation values (Epoch: 2026-09-21T12:54:02.452Z)
Latitude
0.00001°
Longitude
144.06375°
Altitude
537.134 km
Speed
7.594 km/s
True Right ascension
22h 31m 57s
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
15:36:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
540.694 km
Perigee altitude
522.031 km
Semi-major axis
6,909.5 km
Eccentricity
0.00135
Inclination
97.5465°
RAAN
337.9899°
Arg. of periapsis
271.9932°
True anomaly
88.12977°
Mean anomaly
87.9751°
Eccentric anomaly
88.05243°
Mean motion
3.77897 °/min
Orbital period
95.26 mins
BSTAR
0.0001736
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Other satellites on launch #220 in the year 2026 (2026-09-21 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 | 2026-09-22 04:55:00.087Z | 160.463° S | 2026-09-22 04:59:00.087Z | 28.533° NE | 66.864° | 2026-09-22 05:02:00.087Z | 352.459° N |
| 5 mins | 2026-09-22 18:06:00.087Z | 357.39° N | 2026-09-22 18:08:00.087Z | 277.319° WNW | 63.258° | 2026-09-22 18:11:00.087Z | 205.684° 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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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