CENTISPACE-2 S4 is a payload in LEO orbit, operated by Beijing Future Navigation Technology Co. Ltd., launched 2026.
| Orbit class | LEO |
| Inclination | 54.9842° |
| Eccentricity | 0.0010560 |
| Period | 98.6 min |
| Apogee | 700 km |
| Perigee | 685 km |
| Mean motion | 14.60247777 rev/day |
| RAAN | 318.5495° |
| Arg of perigee | 279.0997° |
| Mean anomaly | 80.8801° |
| B* | 1.6388e-4 |
| Rev at epoch | 1,562 |
1 68353U 26060D 26187.79449667 .00000612 00000-0 16388-3 0 99932 68353 54.9842 318.5495 0010560 279.0997 80.8801 14.60247777 15623{
"OBJECT_NAME": "CENTISPACE-2 S4",
"OBJECT_ID": "2026-060D",
"EPOCH": "2026-07-06T19:04:04.512+00:00",
"MEAN_MOTION": 14.60247777,
"ECCENTRICITY": 0.001056,
"INCLINATION": 54.9842,
"RA_OF_ASC_NODE": 318.5495,
"ARG_OF_PERICENTER": 279.0997,
"MEAN_ANOMALY": 80.8801,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 68353,
"REV_AT_EPOCH": 1562,
"BSTAR": 0.00016388,
"MEAN_MOTION_DOT": 0.00000612,
"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-2 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 |