OBJECT E, 64052
Orbit data source: Space-Track
OBJECT E, 64052 is a satellite owned by Youdian Daxue (CN) in SSO that was launched on Sat, 17 May 2025 UTC via a ZHUQUE-2E 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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64052 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Changsha Tianyi
Mission
Operational Amateur Technology
Bus & Motor
TY, Unknown motor
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.255 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 OBJECT E
1 64052U 25103E 26150.21802944 .00015070 00000-0 63370-3 0 9997
2 64052 97.3755 222.9737 0002154 198.5350 161.5809 15.23496768 57373Epoch: 2026-05-30T05:13Z
TLE epoch observation values (Epoch: 2026-05-30T05:13:57.743Z)
Latitude
-0.00003°
Longitude
-103.25411°
Altitude
499.804 km
Speed
7.614 km/s
True Right ascension
14h 51m 53s
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
19:45:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
493.743 km
Perigee altitude
490.783 km
Semi-major axis
6,870.4 km
Eccentricity
0.00022
Inclination
97.3755°
RAAN
222.9737°
Arg. of periapsis
198.535°
True anomaly
161.5887°
Mean anomaly
161.5809°
Eccentric anomaly
161.5848°
Mean motion
3.81127 °/min
Orbital period
94.46 mins
BSTAR
0.0006337
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Other satellites on launch #103 in the year 2025 (2025-05-17 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-30 16:51:26.537Z | 61.968° ENE | 2026-05-30 16:53:26.537Z | 101.954° ESE | 16.757° | 2026-05-30 16:55:26.537Z | 136.47° SSE |
| 4 mins | 2026-05-30 18:25:26.537Z | 322.023° NNW | 2026-05-30 18:26:26.537Z | 297.025° NW | 23.219° | 2026-05-30 18:29:26.537Z | 234.777° WSW |
| 5 mins | 2026-05-31 05:01:26.537Z | 179.026° S | 2026-05-31 05:03:26.537Z | 301.222° NW | 42.789° | 2026-05-31 05:06:26.537Z | 343.648° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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