GONETS-M 10 is a payload in LEO orbit, operated by Gonets Satellite Systems, launched 2014.
| Orbit class | LEO |
| Inclination | 82.5124° |
| Eccentricity | 0.0022997 |
| Period | 115.9 min |
| Apogee | 1,512 km |
| Perigee | 1,476 km |
| Mean motion | 12.42946988 rev/day |
| RAAN | 295.2487° |
| Arg of perigee | 98.9901° |
| Mean anomaly | 261.3783° |
| B* | 1.7060e-3 |
| Rev at epoch | 54,473 |
1 40063U 14036C 26188.19378866 .00000247 00000-0 17060-2 0 99992 40063 82.5124 295.2487 0022997 98.9901 261.3783 12.42946988544735{
"OBJECT_NAME": "GONETS-M 10",
"OBJECT_ID": "2014-036C",
"EPOCH": "2026-07-07T04:39:03.34+00:00",
"MEAN_MOTION": 12.42946988,
"ECCENTRICITY": 0.0022997,
"INCLINATION": 82.5124,
"RA_OF_ASC_NODE": 295.2487,
"ARG_OF_PERICENTER": 98.9901,
"MEAN_ANOMALY": 261.3783,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 40063,
"REV_AT_EPOCH": 54473,
"BSTAR": 0.001706,
"MEAN_MOTION_DOT": 0.00000247,
"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 | GONETS-M 10 |
| Operator | |
| Country | Russia |
| 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 |