YAOGAN-35 03A is a payload in VLEO orbit, operated by General Armaments Dept. of the PLA, launched 2022.
Orbital data last updated 7 days ago. This may not reflect the current orbital state — not for operational use or collision avoidance.
| Orbit class | VLEO |
| Inclination | 35.0076° |
| Eccentricity | 0.0003678 |
| Period | 88.0 min |
| Apogee | 176 km |
| Perigee | 172 km |
| Mean motion | 16.36949118 rev/day |
| RAAN | 309.0104° |
| Arg of perigee | 318.2686° |
| Mean anomaly | 41.7783° |
| B* | 9.3985e-4 |
| Rev at epoch | 22,011 |
This object is recorded as DECAYED (re-entered). These are the last known elements before re-entry — not a current orbit.
1 53316U 22088A 26180.62276802 .09384115 14245-5 93985-3 0 99972 53316 35.0076 309.0104 0003678 318.2686 41.7783 16.36949118220110{
"OBJECT_NAME": "YAOGAN-35 03A",
"OBJECT_ID": "2022-088A",
"EPOCH": "2026-06-29T14:56:47.157+00:00",
"MEAN_MOTION": 16.36949118,
"ECCENTRICITY": 0.0003678,
"INCLINATION": 35.0076,
"RA_OF_ASC_NODE": 309.0104,
"ARG_OF_PERICENTER": 318.2686,
"MEAN_ANOMALY": 41.7783,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 53316,
"REV_AT_EPOCH": 22011,
"BSTAR": 0.00093985,
"MEAN_MOTION_DOT": 0.09384115,
"MEAN_MOTION_DDOT": 0.0000014245
}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-35 03A |
| 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 |
| Decay date |