BEIDOU-3 M10 is a payload in MEO orbit, operated by China National Space Administration, launched 2018.
| Orbit class | MEO |
| Inclination | 54.1743° |
| Eccentricity | 0.0003288 |
| Period | 773.2 min |
| Apogee | 21,537 km |
| Perigee | 21,519 km |
| Mean motion | 1.86229590 rev/day |
| RAAN | 299.3476° |
| Arg of perigee | 34.7932° |
| Mean anomaly | 325.2560° |
| B* | 0.0000e+0 |
| Rev at epoch | 5,621 |
1 43246U 18029B 26186.13958436 -.00000057 00000-0 00000-0 0 99942 43246 54.1743 299.3476 0003288 34.7932 325.2560 1.86229590 56213{
"OBJECT_NAME": "BEIDOU-3 M10",
"OBJECT_ID": "2018-029B",
"EPOCH": "2026-07-05T03:21:00.089+00:00",
"MEAN_MOTION": 1.8622959,
"ECCENTRICITY": 0.0003288,
"INCLINATION": 54.1743,
"RA_OF_ASC_NODE": 299.3476,
"ARG_OF_PERICENTER": 34.7932,
"MEAN_ANOMALY": 325.256,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 43246,
"REV_AT_EPOCH": 5621,
"BSTAR": 0,
"MEAN_MOTION_DOT": -5.7e-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 | BEIDOU-3 M10 |
| Operator | |
| Country | China |
| Launch date | |
| Launch mass (kg) | |
| Mission purpose | — |
| Object class |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Orbital regime |
| Status |