CHUANGXIN 16B (CX-16B) is a payload in LEO orbit, operated by Institute of Microsatellite Innovation, CAS, launched 2022.
| Orbit class | LEO |
| Inclination | 28.9908° |
| Eccentricity | 0.0001136 |
| Period | 93.1 min |
| Apogee | 426 km |
| Perigee | 425 km |
| Mean motion | 15.47067901 rev/day |
| RAAN | 54.8116° |
| Arg of perigee | 329.0542° |
| Mean anomaly | 31.0001° |
| B* | 7.3780e-4 |
| Rev at epoch | 20,975 |
1 53876U 22102B 26187.83951546 .00039052 00000-0 73780-3 0 99982 53876 28.9908 54.8116 0001136 329.0542 31.0001 15.47067901209756{
"OBJECT_NAME": "CHUANGXIN 16B (CX-16B)",
"OBJECT_ID": "2022-102B",
"EPOCH": "2026-07-06T20:08:54.136+00:00",
"MEAN_MOTION": 15.47067901,
"ECCENTRICITY": 0.0001136,
"INCLINATION": 28.9908,
"RA_OF_ASC_NODE": 54.8116,
"ARG_OF_PERICENTER": 329.0542,
"MEAN_ANOMALY": 31.0001,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 53876,
"REV_AT_EPOCH": 20975,
"BSTAR": 0.0007378,
"MEAN_MOTION_DOT": 0.00039052,
"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 | CHUANGXIN 16B (CX-16B) |
| Operator | |
| Country | China |
| Launch date | |
| Launch mass (kg) | |
| Mission purpose | — |
| Object class | PAYLOADHIGH |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Orbital regime |
| Status |