METEOR-M2 4 is a payload in SSO orbit, operated by Rosgidromet NITs Planeta / Joint Stock Corp. VNIIEM, launched 2024.
| Orbit class | SSO |
| Inclination | 98.7020° |
| Eccentricity | 0.0008159 |
| Period | 101.2 min |
| Apogee | 823 km |
| Perigee | 811 km |
| Mean motion | 14.22431588 rev/day |
| RAAN | 147.2085° |
| Arg of perigee | 108.7385° |
| Mean anomaly | 251.4679° |
| B* | 2.6288e-5 |
| Rev at epoch | 12,210 |
1 59051U 24039A 26188.16055593 .00000015 00000-0 26288-4 0 99932 59051 98.7020 147.2085 0008159 108.7385 251.4679 14.22431588122108{
"OBJECT_NAME": "METEOR-M2 4",
"OBJECT_ID": "2024-039A",
"EPOCH": "2026-07-07T03:51:12.032+00:00",
"MEAN_MOTION": 14.22431588,
"ECCENTRICITY": 0.0008159,
"INCLINATION": 98.702,
"RA_OF_ASC_NODE": 147.2085,
"ARG_OF_PERICENTER": 108.7385,
"MEAN_ANOMALY": 251.4679,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 59051,
"REV_AT_EPOCH": 12210,
"BSTAR": 0.000026288,
"MEAN_MOTION_DOT": 1.5e-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 | METEOR-M2 4 |
| Operator | Rosgidromet NITs Planeta / Joint Stock Corp. VNIIEMHIGHvia GCAT — Jonathan McDowell's General Catalog |
| Country | Russia |
| Launch date | |
| Launch mass (kg) | |
| Mission purpose | — |
| Object class | PAYLOADHIGH |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Orbital regime |
| Status |