GONETS-M 8 is a payload in LEO orbit, operated by Gonets Satellite Systems, launched 2014.
| Orbit class | LEO |
| Inclination | 82.5121° |
| Eccentricity | 0.0031091 |
| Period | 115.8 min |
| Apogee | 1,518 km |
| Perigee | 1,470 km |
| Mean motion | 12.42986640 rev/day |
| RAAN | 295.1189° |
| Arg of perigee | 105.5477° |
| Mean anomaly | 254.9039° |
| B* | 1.1271e-3 |
| Rev at epoch | 54,494 |
1 40061U 14036A 26188.25020749 .00000167 00000-0 11271-2 0 99972 40061 82.5121 295.1189 0031091 105.5477 254.9039 12.42986640544940{
"OBJECT_NAME": "GONETS-M 8",
"OBJECT_ID": "2014-036A",
"EPOCH": "2026-07-07T06:00:17.927+00:00",
"MEAN_MOTION": 12.4298664,
"ECCENTRICITY": 0.0031091,
"INCLINATION": 82.5121,
"RA_OF_ASC_NODE": 295.1189,
"ARG_OF_PERICENTER": 105.5477,
"MEAN_ANOMALY": 254.9039,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 40061,
"REV_AT_EPOCH": 54494,
"BSTAR": 0.0011271,
"MEAN_MOTION_DOT": 0.00000167,
"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 8 |
| 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 |