GONETS-M 3 is a payload in LEO orbit, operated by Gonets Satellite Systems, launched 2012.
| Orbit class | LEO |
| Inclination | 82.4733° |
| Eccentricity | 0.0017326 |
| Period | 115.7 min |
| Apogee | 1,500 km |
| Perigee | 1,472 km |
| Mean motion | 12.44903216 rev/day |
| RAAN | 52.2973° |
| Arg of perigee | 20.7433° |
| Mean anomaly | 339.4347° |
| B* | -4.8719e-4 |
| Rev at epoch | 63,315 |
1 38734U 12041B 26188.16160122 -.00000059 00000-0 -48719-3 0 99952 38734 82.4733 52.2973 0017326 20.7433 339.4347 12.44903216633153{
"OBJECT_NAME": "GONETS-M 3",
"OBJECT_ID": "2012-041B",
"EPOCH": "2026-07-07T03:52:42.345+00:00",
"MEAN_MOTION": 12.44903216,
"ECCENTRICITY": 0.0017326,
"INCLINATION": 82.4733,
"RA_OF_ASC_NODE": 52.2973,
"ARG_OF_PERICENTER": 20.7433,
"MEAN_ANOMALY": 339.4347,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 38734,
"REV_AT_EPOCH": 63315,
"BSTAR": -0.00048719,
"MEAN_MOTION_DOT": -5.9e-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 | GONETS-M 3 |
| 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 |