YAOGAN-17 01A is a payload in LEO orbit, operated by General Armaments Dept. of the PLA, launched 2013.
| Orbit class | LEO |
| Inclination | 63.3861° |
| Eccentricity | 0.0427858 |
| Period | 107.0 min |
| Apogee | 1,408 km |
| Perigee | 769 km |
| Mean motion | 13.45510267 rev/day |
| RAAN | 38.5593° |
| Arg of perigee | 12.0050° |
| Mean anomaly | 349.0794° |
| B* | 1.5914e-4 |
| Rev at epoch | 63,098 |
1 39239U 13046A 26188.22140961 .00000074 00000-0 15914-3 0 99942 39239 63.3861 38.5593 0427858 12.0050 349.0794 13.45510267630986{
"OBJECT_NAME": "YAOGAN-17 01A",
"OBJECT_ID": "2013-046A",
"EPOCH": "2026-07-07T05:18:49.79+00:00",
"MEAN_MOTION": 13.45510267,
"ECCENTRICITY": 0.0427858,
"INCLINATION": 63.3861,
"RA_OF_ASC_NODE": 38.5593,
"ARG_OF_PERICENTER": 12.005,
"MEAN_ANOMALY": 349.0794,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 39239,
"REV_AT_EPOCH": 63098,
"BSTAR": 0.00015914,
"MEAN_MOTION_DOT": 7.4e-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-17 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 |