SHENZHOU-22 is a payload in LEO orbit, operated by China Manned Space Engineering Office, launched 2025.
Orbital data last updated 46 days ago. This may not reflect the current orbital state — not for operational use or collision avoidance.
| Orbit class | LEO |
| Inclination | 41.4679° |
| Eccentricity | 0.0007455 |
| Period | 92.3 min |
| Apogee | 391 km |
| Perigee | 381 km |
| Mean motion | 15.60736689 rev/day |
| RAAN | 120.5221° |
| Arg of perigee | 276.8129° |
| Mean anomaly | 83.1862° |
| B* | 1.3456e-4 |
| Rev at epoch | 28,951 |
1 66645U 25272A 26142.03401770 .00011200 00000-0 13456-3 0 99982 66645 41.4679 120.5221 0007455 276.8129 83.1862 15.60736689289513{
"OBJECT_NAME": "SHENZHOU-22",
"OBJECT_ID": "2025-272A",
"EPOCH": "2026-05-22T00:48:59.129+00:00",
"MEAN_MOTION": 15.60736689,
"ECCENTRICITY": 0.00074553,
"INCLINATION": 41.4679,
"RA_OF_ASC_NODE": 120.5221,
"ARG_OF_PERICENTER": 276.8129,
"MEAN_ANOMALY": 83.1862,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 66645,
"REV_AT_EPOCH": 28951,
"BSTAR": 0.00013455509,
"MEAN_MOTION_DOT": 0.000112,
"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 | SHENZHOU-22 |
| Operator | China Manned Space Engineering OfficeHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree |
| Country | |
| Launch date | |
| Launch mass (kg) | 3258 |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Mission purpose | — |
| Object class |
| Orbital regime |
| Status |