YAOGAN-9 01B is a payload in LEO orbit, operated by General Armaments Dept. of the PLA, launched 2010.
| Orbit class | LEO |
| Inclination | 63.3673° |
| Eccentricity | 0.0539785 |
| Period | 107.0 min |
| Apogee | 1,491 km |
| Perigee | 685 km |
| Mean motion | 13.45712155 rev/day |
| RAAN | 307.3015° |
| Arg of perigee | 21.0571° |
| Mean anomaly | 341.1784° |
| B* | 3.0892e-5 |
| Rev at epoch | 80,237 |
1 36414U 10009B 26187.72313411 -.00000048 00000-0 30892-4 0 99932 36414 63.3673 307.3015 0539785 21.0571 341.1784 13.45712155802372{
"OBJECT_NAME": "YAOGAN-9 01B",
"OBJECT_ID": "2010-009B",
"EPOCH": "2026-07-06T17:21:18.787+00:00",
"MEAN_MOTION": 13.45712155,
"ECCENTRICITY": 0.0539785,
"INCLINATION": 63.3673,
"RA_OF_ASC_NODE": 307.3015,
"ARG_OF_PERICENTER": 21.0571,
"MEAN_ANOMALY": 341.1784,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 36414,
"REV_AT_EPOCH": 80237,
"BSTAR": 0.000030892,
"MEAN_MOTION_DOT": -4.8e-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-9 01B |
| 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 |