YAOGAN-20 01A is a payload in LEO orbit, operated by General Armaments Dept. of the PLA, launched 2014.
| Orbit class | LEO |
| Inclination | 63.3807° |
| Eccentricity | 0.0391729 |
| Period | 107.0 min |
| Apogee | 1,382 km |
| Perigee | 797 km |
| Mean motion | 13.45443245 rev/day |
| RAAN | 327.7241° |
| Arg of perigee | 14.7957° |
| Mean anomaly | 346.4153° |
| B* | 1.5254e-5 |
| Rev at epoch | 58,512 |
1 40109U 14047A 26188.13125831 -.00000076 00000-0 15254-4 0 99942 40109 63.3807 327.7241 0391729 14.7957 346.4153 13.45443245585125{
"OBJECT_NAME": "YAOGAN-20 01A",
"OBJECT_ID": "2014-047A",
"EPOCH": "2026-07-07T03:09:00.718+00:00",
"MEAN_MOTION": 13.45443245,
"ECCENTRICITY": 0.0391729,
"INCLINATION": 63.3807,
"RA_OF_ASC_NODE": 327.7241,
"ARG_OF_PERICENTER": 14.7957,
"MEAN_ANOMALY": 346.4153,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 40109,
"REV_AT_EPOCH": 58512,
"BSTAR": 0.000015254,
"MEAN_MOTION_DOT": -7.6e-7,
"MEAN_MOTION_DDOT": 0
}Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.
| Name | YAOGAN-20 01A |
| Operator | |
| Country | China |
| Launch date | |
| Launch mass (kg) | |
| Mission purpose | — |
| Object class |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Orbital regime |
| Status |