DUMMY MASS 4, 69096 (Decayed)
Orbit data source: Space-Track
DUMMY MASS 4, 69096 was a payload satellite owned by Youdian Daxue (CN) in LEO that was launched on Wed, 13 May 2026 UTC via a ZHUQUE-2E launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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69096 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Changsha Tianyi
Mission
Decayed spacecraft
Bus & Motor
TY, Unknown motor
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 DUMMY MASS 4
1 69096U 26105B 26136.59256115 .21767838 11068-6 27752-1 0 9994
2 69096 88.9609 198.4943 0273860 58.5544 304.2185 15.63461160 373Epoch: 2026-05-16T14:13Z
TLE epoch observation values (Epoch: 2026-05-16T14:13:17.283Z)
Latitude
-0.00001°
Longitude
110.86498°
Altitude
280.402 km
Speed
7.796 km/s
True Right ascension
13h 13m 58s
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
13:16:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
559.339 km
Perigee altitude
189.488 km
Semi-major axis
6,752.55 km
Eccentricity
0.02739
Inclination
88.9609°
RAAN
198.4943°
Arg. of periapsis
58.5544°
True anomaly
301.57357°
Mean anomaly
304.2185°
Eccentric anomaly
302.90107°
Mean motion
3.91148 °/min
Orbital period
92.04 mins
BSTAR
0.027752
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Other satellites on launch #105 in the year 2026 (2026-05-13 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.DUMMY MASS 4 Visibility
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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. |
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| This satellite is decayed. |
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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