OBJECT E, 100655
Orbit data source: Space-Track
OBJECT E, 100655 is a satellite owned by PLA SSF (CN) in LEO that was launched on Thu, 10 Sep 2026 UTC via a CHANG ZHENG 4B 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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100655 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
Launch site
Object type
Unknown
Shape & HBR
BOX + 2 PAN, 1.1 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 OBJECT E
1 A0655U 26205E 26286.29501380 .00004546 00000-0 24124-3 0 9998
2 A0655 44.9937 291.5700 0004132 104.5637 255.5701 15.16702217 5006Epoch: 2026-10-13T07:04Z
TLE epoch observation values (Epoch: 2026-10-13T07:04:49.192Z)
Latitude
0.00004°
Longitude
163.50394°
Altitude
516.524 km
Speed
7.607 km/s
True Right ascension
19h 26m 16s
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
15:14:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
520.268 km
Perigee altitude
514.569 km
Semi-major axis
6,895.555 km
Eccentricity
0.00041
Inclination
44.9937°
RAAN
291.57°
Arg. of periapsis
104.5637°
True anomaly
255.52425°
Mean anomaly
255.5701°
Eccentric anomaly
255.54717°
Mean motion
3.79044 °/min
Orbital period
94.98 mins
BSTAR
0.00024124
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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 E 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 | 2026-10-15 03:34:09.591Z | 230.942° WSW | 2026-10-15 03:36:09.591Z | 190.981° SSW | 63.157° | 2026-10-15 03:40:09.591Z | 70.004° E |
| 5 mins | 2026-10-15 05:14:09.591Z | 289.889° WNW | 2026-10-15 05:16:09.591Z | 347.35° N | 43.457° | 2026-10-15 05:19:09.591Z | 58.394° ENE |
| 5 mins | 2026-10-15 06:54:09.591Z | 309.874° NW | 2026-10-15 06:56:09.591Z | 6.219° NNE | 42.079° | 2026-10-15 06:59:09.591Z | 76.401° E |
| 6 mins | 2026-10-15 08:33:09.591Z | 289.854° WNW | 2026-10-15 08:36:09.591Z | 171.032° S | 71.887° | 2026-10-15 08:39:09.591Z | 122.628° SE |
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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