OBJECT E, 100827
Orbit data source: Space-Track
OBJECT E, 100827 is a Chinese satellite in LEO that was launched on Sun, 27 Sep 2026 UTC launched 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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100827 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: 8 hours ago
TLE from 8 hours ago
0 OBJECT E
1 A0827U 26222E 26269.58674455 .00000492 00000-0 19433-3 0 9998
2 A0827 85.9965 70.4790 0010058 266.7416 93.2625 14.26962035 302Epoch: 2026-09-26T14:04Z
TLE epoch observation values (Epoch: 2026-09-26T14:04:54.729Z)
Latitude
0.00004°
Longitude
-146.14171°
Altitude
805.357 km
Speed
7.45 km/s
True Right ascension
04h 41m 54s
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
15:19:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
806.105 km
Perigee altitude
791.668 km
Semi-major axis
7,177.024 km
Eccentricity
0.00101
Inclination
85.9965°
RAAN
70.479°
Arg. of periapsis
266.7416°
True anomaly
93.37756°
Mean anomaly
93.2625°
Eccentric anomaly
93.32003°
Mean motion
3.56966 °/min
Orbital period
100.85 mins
BSTAR
0.00019433
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Other satellites on launch #222 in the year 2026 (2026-09-27 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-09-26 23:04:31.971Z | 355.167° N | 2026-09-26 23:09:31.971Z | 204.629° SW | 75.465° | 2026-09-26 23:13:31.971Z | 181.74° SSW |
| 6 mins | 2026-09-27 10:25:31.971Z | 118.9° SE | 2026-09-27 10:27:31.971Z | 89.922° E | 24.002° | 2026-09-27 10:31:31.971Z | 34.922° NE |
| 8 mins | 2026-09-27 12:05:31.971Z | 219.615° SW | 2026-09-27 12:08:31.971Z | 266.445° W | 37.4° | 2026-09-27 12:13:31.971Z | 344.591° N |
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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