METEOR-M 2 is a payload in SSO orbit, operated by Rosgidromet NITs Planeta / Joint Stock Corp. VNIIEM, launched 2014.
| Orbit class | SSO |
| Inclination | 98.5129° |
| Eccentricity | 0.0005674 |
| Period | 101.3 min |
| Apogee | 825 km |
| Perigee | 816 km |
| Mean motion | 14.21468143 rev/day |
| RAAN | 163.2372° |
| Arg of perigee | 351.6102° |
| Mean anomaly | 8.4980° |
| B* | 1.8663e-4 |
| Rev at epoch | 62,216 |
1 40069U 14037A 26188.20672045 .00000366 00000-0 18663-3 0 99972 40069 98.5129 163.2372 0005674 351.6102 8.4980 14.21468143622169{
"OBJECT_NAME": "METEOR-M 2",
"OBJECT_ID": "2014-037A",
"EPOCH": "2026-07-07T04:57:40.647+00:00",
"MEAN_MOTION": 14.21468143,
"ECCENTRICITY": 0.0005674,
"INCLINATION": 98.5129,
"RA_OF_ASC_NODE": 163.2372,
"ARG_OF_PERICENTER": 351.6102,
"MEAN_ANOMALY": 8.498,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 40069,
"REV_AT_EPOCH": 62216,
"BSTAR": 0.00018663,
"MEAN_MOTION_DOT": 0.00000366,
"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-M 2 |
| 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 |