CENTISPACE-2 S1 is a payload in LEO orbit, operated by Beijing Future Navigation Technology Co. Ltd., launched 2026.
| Orbit class | LEO |
| Inclination | 54.9826° |
| Eccentricity | 0.0006504 |
| Period | 98.6 min |
| Apogee | 697 km |
| Perigee | 688 km |
| Mean motion | 14.60336513 rev/day |
| RAAN | 317.4083° |
| Arg of perigee | 280.6750° |
| Mean anomaly | 79.3510° |
| B* | 1.2364e-4 |
| Rev at epoch | 1,566 |
1 68350U 26060A 26188.06228536 .00000418 00000-0 12364-3 0 99952 68350 54.9826 317.4083 0006504 280.6750 79.3510 14.60336513 15662{
"OBJECT_NAME": "CENTISPACE-2 S1",
"OBJECT_ID": "2026-060A",
"EPOCH": "2026-07-07T01:29:41.455+00:00",
"MEAN_MOTION": 14.60336513,
"ECCENTRICITY": 0.0006504,
"INCLINATION": 54.9826,
"RA_OF_ASC_NODE": 317.4083,
"ARG_OF_PERICENTER": 280.675,
"MEAN_ANOMALY": 79.351,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 68350,
"REV_AT_EPOCH": 1566,
"BSTAR": 0.00012364,
"MEAN_MOTION_DOT": 0.00000418,
"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 S1 |
| 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 |