GONETS-M 12 is a payload in LEO orbit, operated by Gonets Satellite Systems, launched 2015.
| Orbit class | LEO |
| Inclination | 82.4896° |
| Eccentricity | 0.0014444 |
| Period | 115.9 min |
| Apogee | 1,506 km |
| Perigee | 1,483 km |
| Mean motion | 12.42891657 rev/day |
| RAAN | 19.6560° |
| Arg of perigee | 306.0872° |
| Mean anomaly | 53.8869° |
| B* | -4.3308e-4 |
| Rev at epoch | 51,121 |
1 40553U 15020B 26188.18652219 -.00000050 00000-0 -43308-3 0 99922 40553 82.4896 19.6560 0014444 306.0872 53.8869 12.42891657511210{
"OBJECT_NAME": "GONETS-M 12",
"OBJECT_ID": "2015-020B",
"EPOCH": "2026-07-07T04:28:35.517+00:00",
"MEAN_MOTION": 12.42891657,
"ECCENTRICITY": 0.0014444,
"INCLINATION": 82.4896,
"RA_OF_ASC_NODE": 19.656,
"ARG_OF_PERICENTER": 306.0872,
"MEAN_ANOMALY": 53.8869,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 40553,
"REV_AT_EPOCH": 51121,
"BSTAR": -0.00043308,
"MEAN_MOTION_DOT": -5e-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 12 |
| 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 |