OBJECT A, 64048

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 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.

Loading next visibility...
Identifier
64048, 2025-103A
Orbit
SSO
Last TLE update
4 hours ago
Origin
Flag of CNCTYK/CUGW (CN / PRC)
Manufacturer
Changsha Tianyi
Mission
Operational Commercial Imaging
Bus & Motor
TY, Unknown motor
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
2025-05-17 (2 months ago)
Launch vehicle
ZHUQUE-2E
Launch site
Jiuquan Satellite Launch Center, China (JSC)
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 4 hours ago
0 OBJECT A
1 64048U 25103A   25200.16718037  .00005167  00000-0  27786-3 0  9997
2 64048  97.4122 274.2524 0002773 278.1260  81.9658 15.15299052  9533
Epoch: 2025-07-19T04:00Z
TLE epoch observation values (Epoch: 2025-07-19T04:00:44.383Z)
Latitude
-0.00005°
Longitude
-83.1407°
Altitude
522.888 km
Speed
7.602 km/s
True Right ascension
18h 17m 00s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
-49.8034°
Longitude
88.22152°
Altitude
538.141 km
Speed
7.593 km/s
Apparent Right ascension
07h 26m 24s
Apparent Declination
-47° 38' 08"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
21:00:44
Azimuth
122.303° SE
Elevation
-71.403°
Doppler factor
1
Orbital elements
Apogee altitude
518.955 km
Perigee altitude
515.131 km
Semi-major axis
6,895.18 km
Eccentricity
0.00028
Inclination
97.4122°
RAAN
274.2524°
Arg. of periapsis
278.126°
True anomaly
81.99727°
Mean anomaly
81.9658°
Eccentric anomaly
81.98153°
Mean motion
3.79075 °/min
Orbital period
94.97 mins
BSTAR
0.00027786
Loading maneuver chart data...
Loading SW <> Apogee altitude chart data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
|