BEIDOU-2 G4 is a payload in GEO orbit, operated by China National Space Administration, launched 2010.
| Orbit class | GEO |
| Inclination | 3.6931° |
| Eccentricity | 0.0005114 |
| Period | 1436.1 min |
| Apogee | 35,808 km |
| Perigee | 35,765 km |
| Mean motion | 1.00270870 rev/day |
| RAAN | 68.8267° |
| Arg of perigee | 186.2567° |
| Mean anomaly | 227.9115° |
| B* | 0.0000e+0 |
| Rev at epoch | 5,749 |
1 37210U 10057A 26188.10542397 -.00000100 00000-0 00000-0 0 99942 37210 3.6931 68.8267 0005114 186.2567 227.9115 1.00270870 57497{
"OBJECT_NAME": "BEIDOU-2 G4",
"OBJECT_ID": "2010-057A",
"EPOCH": "2026-07-07T02:31:48.631+00:00",
"MEAN_MOTION": 1.0027087,
"ECCENTRICITY": 0.0005114,
"INCLINATION": 3.6931,
"RA_OF_ASC_NODE": 68.8267,
"ARG_OF_PERICENTER": 186.2567,
"MEAN_ANOMALY": 227.9115,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 37210,
"REV_AT_EPOCH": 5749,
"BSTAR": 0,
"MEAN_MOTION_DOT": -0.000001,
"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-2 G4 |
| 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 |