OBJECT A, 100465
Orbit data source: Space-Track
OBJECT A, 100465 is a Chinese satellite in SSO that was launched on Tue, 25 Aug 2026 UTC via a CHANG ZHENG 6C launch vehicle from the Taiyaun Space Center, China (TSC). 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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100465 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
ASES/SAST
Mission
Operational Amateur Communications
Bus & Motor
JAMX, Unknown motor
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 2 Pan, 1.1 m
Radar Cross Section
0.195 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 OBJECT A
1 A0465U 26195A 26295.78911434 .00004901 00000-0 31536-3 0 9994
2 A0465 97.5350 8.5856 0012420 61.8639 298.3843 15.08777553 8845Epoch: 2026-10-22T18:56Z
TLE epoch observation values (Epoch: 2026-10-22T18:56:19.478Z)
Latitude
-0.00007°
Longitude
53.28548°
Altitude
538.928 km
Speed
7.595 km/s
True Right ascension
00h 34m 20s
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
06:14:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
545.509 km
Perigee altitude
528.332 km
Semi-major axis
6,915.058 km
Eccentricity
0.00124
Inclination
97.535°
RAAN
8.5856°
Arg. of periapsis
61.8639°
True anomaly
298.259°
Mean anomaly
298.3843°
Eccentric anomaly
298.32166°
Mean motion
3.77441 °/min
Orbital period
95.38 mins
BSTAR
0.00031536
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Other satellites on launch #195 in the year 2026 (2026-08-25 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 | 2026-10-23 17:46:55.481Z | 15.235° NNE | 2026-10-23 17:49:55.481Z | 40.306° NE | 66.773° | 2026-10-23 17:53:55.481Z | 188.628° SSW |
| 5 mins | 2026-10-24 04:30:55.481Z | 123.878° SE | 2026-10-24 04:32:55.481Z | 71.189° E | 34.875° | 2026-10-24 04:35:55.481Z | 9.57° NNE |
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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