GONETS-M 25 is a payload in LEO orbit, operated by Gonets Satellite Systems, launched 2022.
| Orbit class | LEO |
| Inclination | 82.5069° |
| Eccentricity | 0.0020777 |
| Period | 115.9 min |
| Apogee | 1,511 km |
| Perigee | 1,478 km |
| Mean motion | 12.42890670 rev/day |
| RAAN | 335.6085° |
| Arg of perigee | 184.2996° |
| Mean anomaly | 175.7908° |
| B* | 2.1031e-4 |
| Rev at epoch | 16,813 |
1 54152U 22139C 26188.18550316 .00000039 00000-0 21031-3 0 99902 54152 82.5069 335.6085 0020777 184.2996 175.7908 12.42890670168136{
"OBJECT_NAME": "GONETS-M 25",
"OBJECT_ID": "2022-139C",
"EPOCH": "2026-07-07T04:27:07.473+00:00",
"MEAN_MOTION": 12.4289067,
"ECCENTRICITY": 0.0020777,
"INCLINATION": 82.5069,
"RA_OF_ASC_NODE": 335.6085,
"ARG_OF_PERICENTER": 184.2996,
"MEAN_ANOMALY": 175.7908,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 54152,
"REV_AT_EPOCH": 16813,
"BSTAR": 0.00021031,
"MEAN_MOTION_DOT": 3.9e-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 25 |
| 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 |