CENTISPACE-1 S14 is a payload in LEO orbit, operated by Beijing Future Navigation Technology Co. Ltd., launched 2025.
| Orbit class | LEO |
| Inclination | 54.9822° |
| Eccentricity | 0.0012441 |
| Period | 104.3 min |
| Apogee | 971 km |
| Perigee | 953 km |
| Mean motion | 13.80614662 rev/day |
| RAAN | 222.6425° |
| Arg of perigee | 127.0884° |
| Mean anomaly | 233.1212° |
| B* | 4.2894e-5 |
| Rev at epoch | 7,747 |
1 62583U 25007J 26188.19040028 -.00000095 00000-0 42894-4 0 99932 62583 54.9822 222.6425 0012441 127.0884 233.1212 13.80614662 77477{
"OBJECT_NAME": "CENTISPACE-1 S14",
"OBJECT_ID": "2025-007J",
"EPOCH": "2026-07-07T04:34:10.584+00:00",
"MEAN_MOTION": 13.80614662,
"ECCENTRICITY": 0.0012441,
"INCLINATION": 54.9822,
"RA_OF_ASC_NODE": 222.6425,
"ARG_OF_PERICENTER": 127.0884,
"MEAN_ANOMALY": 233.1212,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 62583,
"REV_AT_EPOCH": 7747,
"BSTAR": 0.000042894,
"MEAN_MOTION_DOT": -9.5e-7,
"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 S14 |
| 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 |