OBJECT E, 69542
Orbit data source: Space-Track
OBJECT E, 69542 is a Chinese satellite in SSO that was launched on Mon, 15 Jun 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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69542 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
Launch site
Object type
Unknown
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 OBJECT E
1 69542U 26134E 26166.46458882 .00001398 00000-0 91299-4 0 9993
2 69542 97.7040 236.5599 0014779 282.3968 77.5607 15.09464710 43Epoch: 2026-06-15T11:09Z
TLE epoch observation values (Epoch: 2026-06-15T11:09:00.474Z)
Latitude
0.00007°
Longitude
165.55732°
Altitude
538.714 km
Speed
7.594 km/s
True Right ascension
15h 46m 14s
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
04:50:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
545.044 km
Perigee altitude
524.611 km
Semi-major axis
6,912.964 km
Eccentricity
0.00148
Inclination
97.704°
RAAN
236.5599°
Arg. of periapsis
282.3968°
True anomaly
77.72614°
Mean anomaly
77.5607°
Eccentric anomaly
77.64342°
Mean motion
3.77613 °/min
Orbital period
95.34 mins
BSTAR
0.000091299
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Other satellites on launch #134 in the year 2026 (2026-06-15 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 | 2026-06-17 04:38:12.332Z | 162.442° S | 2026-06-17 04:41:12.332Z | 140.174° SSE | 42.791° | 2026-06-17 04:45:12.332Z | 350.378° N |
| 6 mins | 2026-06-17 17:49:12.332Z | 358.256° N | 2026-06-17 17:51:12.332Z | 306.969° NW | 40.327° | 2026-06-17 17:55:12.332Z | 205.691° 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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