OBJECT A, 64048
Orbit data source: Space-Track
OBJECT A, 64048 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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64048 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Changsha Tianyi
Mission
Operational Amateur Imaging
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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 OBJECT A
1 64048U 25103A 26150.12708606 .00002025 00000-0 99488-4 0 9998
2 64048 97.4120 223.0217 0001632 89.7973 270.3448 15.19180849 57331Epoch: 2026-05-30T03:03Z
TLE epoch observation values (Epoch: 2026-05-30T03:03:00.235Z)
Latitude
-0.0001°
Longitude
-70.37685°
Altitude
511.397 km
Speed
7.608 km/s
True Right ascension
14h 52m 05s
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
19:45:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.406 km
Perigee altitude
504.159 km
Semi-major axis
6,883.419 km
Eccentricity
0.00016
Inclination
97.412°
RAAN
223.0217°
Arg. of periapsis
89.7973°
True anomaly
270.3261°
Mean anomaly
270.3448°
Eccentric anomaly
270.33545°
Mean motion
3.80047 °/min
Orbital period
94.73 mins
BSTAR
0.000099488
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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 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 | 2026-05-30 17:50:36.703Z | 6.472° NNE | 2026-05-30 17:53:36.703Z | 241.518° WSW | 42.983° | 2026-05-30 17:56:36.703Z | 199.43° SSW |
| 5 mins | 2026-05-31 04:29:36.703Z | 129.705° SE | 2026-05-31 04:31:36.703Z | 67.854° E | 32.691° | 2026-05-31 04:34:36.703Z | 5.413° NNE |
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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