CENTISPACE-1 S4 is a payload in LEO orbit, operated by Beijing Future Navigation Technology Co. Ltd., launched 2022.
| Orbit class | LEO |
| Inclination | 53.5317° |
| Eccentricity | 0.0009741 |
| Period | 98.5 min |
| Apogee | 694 km |
| Perigee | 680 km |
| Mean motion | 14.61964275 rev/day |
| RAAN | 330.1119° |
| Arg of perigee | 35.3404° |
| Mean anomaly | 324.8216° |
| B* | 1.4541e-4 |
| Rev at epoch | 20,448 |
1 53758U 22108B 26188.15519155 .00000544 00000-0 14541-3 0 99992 53758 53.5317 330.1119 0009741 35.3404 324.8216 14.61964275204481{
"OBJECT_NAME": "CENTISPACE-1 S4",
"OBJECT_ID": "2022-108B",
"EPOCH": "2026-07-07T03:43:28.55+00:00",
"MEAN_MOTION": 14.61964275,
"ECCENTRICITY": 0.0009741,
"INCLINATION": 53.5317,
"RA_OF_ASC_NODE": 330.1119,
"ARG_OF_PERICENTER": 35.3404,
"MEAN_ANOMALY": 324.8216,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 53758,
"REV_AT_EPOCH": 20448,
"BSTAR": 0.00014541,
"MEAN_MOTION_DOT": 0.00000544,
"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 | CENTISPACE-1 S4 |
| 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 |