GONETS-M 9 is a payload in LEO orbit, operated by Gonets Satellite Systems, launched 2014.
| Orbit class | LEO |
| Inclination | 82.5120° |
| Eccentricity | 0.0024346 |
| Period | 115.9 min |
| Apogee | 1,513 km |
| Perigee | 1,475 km |
| Mean motion | 12.42952086 rev/day |
| RAAN | 295.2723° |
| Arg of perigee | 112.0575° |
| Mean anomaly | 248.3094° |
| B* | 9.0225e-4 |
| Rev at epoch | 54,493 |
1 40062U 14036B 26188.13093810 .00000135 00000-0 90225-3 0 99962 40062 82.5120 295.2723 0024346 112.0575 248.3094 12.42952086544936{
"OBJECT_NAME": "GONETS-M 9",
"OBJECT_ID": "2014-036B",
"EPOCH": "2026-07-07T03:08:33.052+00:00",
"MEAN_MOTION": 12.42952086,
"ECCENTRICITY": 0.0024346,
"INCLINATION": 82.512,
"RA_OF_ASC_NODE": 295.2723,
"ARG_OF_PERICENTER": 112.0575,
"MEAN_ANOMALY": 248.3094,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 40062,
"REV_AT_EPOCH": 54493,
"BSTAR": 0.00090225,
"MEAN_MOTION_DOT": 0.00000135,
"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 9 |
| 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 |