GONETS-M 23 is a payload in LEO orbit, operated by Gonets Satellite Systems, launched 2022.
| Orbit class | LEO |
| Inclination | 82.5087° |
| Eccentricity | 0.0021791 |
| Period | 115.9 min |
| Apogee | 1,512 km |
| Perigee | 1,477 km |
| Mean motion | 12.42891598 rev/day |
| RAAN | 335.8400° |
| Arg of perigee | 175.4720° |
| Mean anomaly | 184.6560° |
| B* | 1.7690e-4 |
| Rev at epoch | 16,813 |
1 54150U 22139A 26188.22601502 .00000034 00000-0 17690-3 0 99982 54150 82.5087 335.8400 0021791 175.4720 184.6560 12.42891598168134{
"OBJECT_NAME": "GONETS-M 23",
"OBJECT_ID": "2022-139A",
"EPOCH": "2026-07-07T05:25:27.698+00:00",
"MEAN_MOTION": 12.42891598,
"ECCENTRICITY": 0.0021791,
"INCLINATION": 82.5087,
"RA_OF_ASC_NODE": 335.84,
"ARG_OF_PERICENTER": 175.472,
"MEAN_ANOMALY": 184.656,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 54150,
"REV_AT_EPOCH": 16813,
"BSTAR": 0.0001769,
"MEAN_MOTION_DOT": 3.4e-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 23 |
| 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 |