CHUANGXIN 16A (CX-16A) is a payload in LEO orbit, operated by Institute of Microsatellite Innovation, CAS, launched 2022.
| Orbit class | LEO |
| Inclination | 28.9938° |
| Eccentricity | 0.0004793 |
| Period | 95.6 min |
| Apogee | 552 km |
| Perigee | 545 km |
| Mean motion | 15.05992401 rev/day |
| RAAN | 194.9858° |
| Arg of perigee | 220.5894° |
| Mean anomaly | 139.4348° |
| B* | 9.9100e-5 |
| Rev at epoch | 21,254 |
1 53586U 22102A 26188.20536075 .00001638 00000-0 99100-4 0 99982 53586 28.9938 194.9858 0004793 220.5894 139.4348 15.05992401212547{
"OBJECT_NAME": "CHUANGXIN 16A (CX-16A)",
"OBJECT_ID": "2022-102A",
"EPOCH": "2026-07-07T04:55:43.169+00:00",
"MEAN_MOTION": 15.05992401,
"ECCENTRICITY": 0.0004793,
"INCLINATION": 28.9938,
"RA_OF_ASC_NODE": 194.9858,
"ARG_OF_PERICENTER": 220.5894,
"MEAN_ANOMALY": 139.4348,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 53586,
"REV_AT_EPOCH": 21254,
"BSTAR": 0.0000991,
"MEAN_MOTION_DOT": 0.00001638,
"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 16A (CX-16A) |
| 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 |