GONETS-M 4 is a payload in LEO orbit, operated by Gonets Satellite Systems, launched 2012.
| Orbit class | LEO |
| Inclination | 82.4777° |
| Eccentricity | 0.0025782 |
| Period | 115.8 min |
| Apogee | 1,510 km |
| Perigee | 1,470 km |
| Mean motion | 12.43905000 rev/day |
| RAAN | 58.3451° |
| Arg of perigee | 11.7365° |
| Mean anomaly | 348.4310° |
| B* | 5.7327e-6 |
| Rev at epoch | 62,543 |
1 38736U 12041D 26188.13486411 .00000011 00000-0 57327-5 0 99992 38736 82.4777 58.3451 0025782 11.7365 348.4310 12.43905000625434{
"OBJECT_NAME": "GONETS-M 4",
"OBJECT_ID": "2012-041D",
"EPOCH": "2026-07-07T03:14:12.259+00:00",
"MEAN_MOTION": 12.43905,
"ECCENTRICITY": 0.0025782,
"INCLINATION": 82.4777,
"RA_OF_ASC_NODE": 58.3451,
"ARG_OF_PERICENTER": 11.7365,
"MEAN_ANOMALY": 348.431,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 38736,
"REV_AT_EPOCH": 62543,
"BSTAR": 0.0000057327,
"MEAN_MOTION_DOT": 1.1e-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 4 |
| 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 |