Official name MISRSAT-2
Alternative name Xingchi-1 02A
Cospar ID 2023-187B
Norad ID 58497
Launch date 2023-12-04
Launch site JSC
Launch vehicle CZ-2C (3)
Country/Organization Egypt
Type application Earth Observation
Operator EgSA
RCS size LARGE
Decay date ON ORBIT
Period (min) 97.37
Inclination (deg) 97.99
Perigee (km) 624
Apogee (km) 642
Eccentricity 0.014218009478673
Mean motion (revs. per day) 14.7889493683886
Semi-Major axis (km) 7011.135
Raan (deg) 200.0295
Arg of perigee (deg) 139.8333
Shape Box + 2 Pan
Mass (kg) 35
Height (m) 0.3
Width (m) 0.3
Depth (m) 0.3
Span (m^2) 1
Lifetime 5 years
Contractors CAST (bus)
Equipment Imager
Power 2 deployable fixed solar arrays, batteries

MisrSat 2 (not to be confused with EgyptSat 2 (MisrSat 2) launched in 2014) or Aiji 2 (Aiji Yaogan Weixing Erhao) is an Egyptian Earth remote-sounding satellite, built as a joint project between the Egyptian Space Agency (EgSA) and its Chinese counterpart.

The satellite features an high-resolution imager with a ground resolution of 2 meters in panchromatic mode and 8 meters in color.

The Chinese CAST delivered two prototype and one flight unit of the satellite bus to Egypt, where the Egyptian imaging payload was integrated and tested. Then the flight unit was returned to China for launch.

Satellite COSPAR Date LS Launch Vehicle Remarks
MISRSAT-2 2023-187B 2023-12-04 JSC CZ-2C (3) with Xingchi-1 02A, Xingchi-1 02B