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: 1 day ago
TLE from 1 day ago
0 OBJECT A
1 64048U 25103A 26206.70724112 .00002182 00000-0 10697-3 0 9992
2 64048 97.4122 278.5435 0001715 88.7154 271.4277 15.19178773 65921Epoch: 2026-07-25T16:58Z
TLE epoch observation values (Epoch: 2026-07-25T16:58:25.632Z)
Latitude
-0.00005°
Longitude
80.52105°
Altitude
511.381 km
Speed
7.608 km/s
True Right ascension
18h 34m 10s
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
08:40:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.469 km
Perigee altitude
504.108 km
Semi-major axis
6,883.425 km
Eccentricity
0.00017
Inclination
97.4122°
RAAN
278.5435°
Arg. of periapsis
88.7154°
True anomaly
271.40805°
Mean anomaly
271.4277°
Eccentric anomaly
271.41788°
Mean motion
3.80046 °/min
Orbital period
94.73 mins
BSTAR
0.00010697
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-07-27 05:27:57.992Z | 209.254° SW | 2026-07-27 05:29:57.992Z | 253.934° W | 26.795° | 2026-07-27 05:32:57.992Z | 321.671° NNW |
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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