OBJECT E, 64052
Orbit data source: Space-Track
You're viewing an Uncataloged Satellite
Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
OBJECT E, 64052 is a Chinese satellite 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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Edit Public Description
Identifier
Orbit
Last TLE update
6 hours ago
Origin
CTYK/YOUD (CN / PRC)Manufacturer
Changsha Tianyi
Mission
Operational Commercial 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 & history
TLE from 6 hours ago
0 OBJECT E
1 64052U 25103E 25211.56740666 .00008376 00000-0 43987-3 0 9997
2 64052 97.4128 285.4467 0002992 188.6807 171.4375 15.15953878 11255Epoch: 2025-07-30T13:37Z
TLE epoch observation values (Epoch: 2025-07-30T13:37:03.935Z)
Latitude
0.00001°
Longitude
132.73552°
Altitude
523.21 km
Speed
7.6 km/s
True Right ascension
19h 01m 47s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
-41.43674°
Longitude
139.54454°
Altitude
535.372 km
Speed
7.593 km/s
Apparent Right ascension
20h 23m 09s
Apparent Declination
-41° 22' 19"
Sunlit
Visualization observer readout
Local Sidereal Time
09:20:33
Azimuth
102.264° ESE
Elevation
-79.025°
Doppler factor
1
Orbital elements
Apogee altitude
517.118 km
Perigee altitude
512.993 km
Semi-major axis
6,893.193 km
Eccentricity
0.0003
Inclination
97.4128°
RAAN
285.4467°
Arg. of periapsis
188.6807°
True anomaly
171.4426°
Mean anomaly
171.4375°
Eccentric anomaly
171.44005°
Mean motion
3.79239 °/min
Orbital period
94.93 mins
BSTAR
0.00043987
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Other satellites on launch #103 in the year 2025 (2025-05-17 UTC)
OBJECT E Visibility forecast
Observer location: undefined°, undefined°
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 | 2025-07-31 04:02:14.847Z | 99.671° ESE | 2025-07-31 04:04:14.847Z | 63.472° ENE | 15.856° | 2025-07-31 04:06:14.847Z | 30.038° NE |
| 4 mins | 2025-07-31 05:36:14.847Z | 218.863° SW | 2025-07-31 05:38:14.847Z | 274.847° WNW | 26.926° | 2025-07-31 05:40:14.847Z | 317.487° NNW |
| 4 mins | 2025-07-31 17:08:14.847Z | 54.498° ENE | 2025-07-31 17:10:14.847Z | 99.333° ESE | 22.296° | 2025-07-31 17:12:14.847Z | 140.893° SSE |
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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Authenticating...
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