GONETS-M 5 is a payload in LEO orbit, operated by Gonets Satellite Systems, launched 2013.
| Orbit class | LEO |
| Inclination | 82.4852° |
| Eccentricity | 0.0017001 |
| Period | 115.9 min |
| Apogee | 1,508 km |
| Perigee | 1,481 km |
| Mean motion | 12.42892325 rev/day |
| RAAN | 330.9305° |
| Arg of perigee | 166.5590° |
| Mean anomaly | 193.5946° |
| B* | 1.7781e-4 |
| Rev at epoch | 58,136 |
1 39249U 13048A 26188.15862759 .00000035 00000-0 17781-3 0 99962 39249 82.4852 330.9305 0017001 166.5590 193.5946 12.42892325581360{
"OBJECT_NAME": "GONETS-M 5",
"OBJECT_ID": "2013-048A",
"EPOCH": "2026-07-07T03:48:25.424+00:00",
"MEAN_MOTION": 12.42892325,
"ECCENTRICITY": 0.0017001,
"INCLINATION": 82.4852,
"RA_OF_ASC_NODE": 330.9305,
"ARG_OF_PERICENTER": 166.559,
"MEAN_ANOMALY": 193.5946,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 39249,
"REV_AT_EPOCH": 58136,
"BSTAR": 0.00017781,
"MEAN_MOTION_DOT": 3.5e-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 5 |
| 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 |