OBJECT A, 69097
Orbit data source: Space-Track
OBJECT A, 69097 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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69097 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 shape, 1.1 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 OBJECT A
1 69097U 26106A 26168.80874800 .00004729 00000-0 28466-3 0 9995
2 69097 97.5095 250.8820 0015046 159.1038 201.0810 15.11201508 5074Epoch: 2026-06-17T19:24Z
TLE epoch observation values (Epoch: 2026-06-17T19:24:35.827Z)
Latitude
-0.00002°
Longitude
53.67161°
Altitude
545.316 km
Speed
7.584 km/s
True Right ascension
16h 43m 31s
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
12:30:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
539.91 km
Perigee altitude
519.123 km
Semi-major axis
6,907.654 km
Eccentricity
0.0015
Inclination
97.5095°
RAAN
250.882°
Arg. of periapsis
159.1038°
True anomaly
201.01909°
Mean anomaly
201.081°
Eccentric anomaly
201.05004°
Mean motion
3.78048 °/min
Orbital period
95.23 mins
BSTAR
0.00028466
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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 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-18 05:04:46.303Z | 138.787° SSE | 2026-06-18 05:07:46.303Z | 70.372° E | 32.802° | 2026-06-18 05:10:46.303Z | 6.516° NNE |
| 6 mins | 2026-06-18 18:13:46.303Z | 19.442° NNE | 2026-06-18 18:16:46.303Z | 132.182° SE | 42.53° | 2026-06-18 18:19:46.303Z | 184.506° 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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