OBJECT E, 69101
Orbit data source: Space-Track
OBJECT E, 69101 is a Chinese satellite in SSO that was launched on Fri, 15 May 2026 UTC via a LIJIAN-1 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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Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 OBJECT E
1 69101U 26106E 26135.82908956 .00000497 00000-0 33338-4 0 9990
2 69101 97.5067 218.5063 0013930 282.6221 77.3451 15.11230034 105Epoch: 2026-05-15T19:53Z
TLE epoch observation values (Epoch: 2026-05-15T19:53:53.337Z)
Latitude
-0.00008°
Longitude
46.47928°
Altitude
533.427 km
Speed
7.597 km/s
True Right ascension
14h 34m 01s
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
12:51:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
539.052 km
Perigee altitude
519.807 km
Semi-major axis
6,907.566 km
Eccentricity
0.00139
Inclination
97.5067°
RAAN
218.5063°
Arg. of periapsis
282.6221°
True anomaly
77.50091°
Mean anomaly
77.3451°
Eccentric anomaly
77.423°
Mean motion
3.78055 °/min
Orbital period
95.22 mins
BSTAR
0.000033338
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Other satellites on launch #106 in the year 2026 (2026-05-15 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-18 05:13:37.542Z | 150.682° SSE | 2026-05-18 05:17:37.542Z | 51.349° ENE | 37.523° | 2026-05-18 05:20:37.542Z | 359.407° N |
| 6 mins | 2026-05-18 18:23:37.542Z | 11.561° NNE | 2026-05-18 18:26:37.542Z | 197.128° SSW | 42.981° | 2026-05-18 18:29:37.542Z | 193.814° SSW |
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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