METEOR-M2 3 is a payload in SSO orbit, operated by Rosgidromet NITs Planeta / Joint Stock Corp. VNIIEM, launched 2023.
| Orbit class | SSO |
| Inclination | 98.6077° |
| Eccentricity | 0.0005103 |
| Period | 101.1 min |
| Apogee | 815 km |
| Perigee | 808 km |
| Mean motion | 14.24048492 rev/day |
| RAAN | 242.7614° |
| Arg of perigee | 108.1933° |
| Mean anomaly | 251.9802° |
| B* | 9.9571e-6 |
| Rev at epoch | 15,736 |
1 57166U 23091A 26188.19347610 -.00000020 00000-0 99571-5 0 99952 57166 98.6077 242.7614 0005103 108.1933 251.9802 14.24048492157361{
"OBJECT_NAME": "METEOR-M2 3",
"OBJECT_ID": "2023-091A",
"EPOCH": "2026-07-07T04:38:36.335+00:00",
"MEAN_MOTION": 14.24048492,
"ECCENTRICITY": 0.0005103,
"INCLINATION": 98.6077,
"RA_OF_ASC_NODE": 242.7614,
"ARG_OF_PERICENTER": 108.1933,
"MEAN_ANOMALY": 251.9802,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 57166,
"REV_AT_EPOCH": 15736,
"BSTAR": 0.0000099571,
"MEAN_MOTION_DOT": -2e-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 3 |
| 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 |