Official name TJS-6
Alternative name TJS-6
Cospar ID 2021-010A
Norad ID 47613
Launch date 2021-02-04
Launch site XSC
Launch vehicle CZ-3B/G2
Country/Organization China
Type application Early warning ?
RCS size LARGE
Decay date ON ORBIT
Period (min) 1436.12
Inclination (deg) 0.44
Perigee (km) 35778
Apogee (km) 35796
Eccentricity 0.000251487970492078
Mean motion (revs. per day) 1.00270172408991
Semi-Major axis (km) 42165.135
Raan (deg) 90.2577
Arg of perigee (deg) 111.7683
Shape Box + 2 Pan
Mass (kg) 4000
Height (m) 5
Width (m) 2.5
Depth (m) 2.5
Span (m^2) 30
Contractors SAST
Propulsion ?
Configuration SAST-5000 ?
Power 2 deployable solar arrays, batteries

TJS 2 (Tongxin Jishu Shiyan) is a Chinese geostationary satellite.

The satellite was built by SAST. According to public announcement the satellite will be mainly used to conduct a test on high speed/multi-frequency wide-band data transfer communication.

The lack of public information has lead to the suspiction, that this satellite has a military mission. The published image of the satellite does not fit to a communications satellite. It has been speculated, that it might be in fact a military Huoyan-1 (?) early warning satellite.

The satellite was launched in January 2017.

Another SAST built satellite, TJS 5, was launched on 7 January 2020. It has been speculated to be of the same type as TJS 2, as the generic description, manufacturer and NOTAMs are nearly the same as for TJS 2. A third satellite of this seriers, TJS 6, has been launched on 4 February 2021.

Satellite COSPAR Date LS Launch Vehicle Remarks
TJS-2 2017-001A 2017-01-05 XSC CZ-3B/G2
TJS-5 2020-002A 2020-01-07 XSC CZ-3B/G3
TJS-6 2021-010A 2021-02-04 XSC CZ-3B/G2