METEOR-M2 2 is a payload in SSO orbit, operated by Rosgidromet NITs Planeta / Joint Stock Corp. VNIIEM, launched 2019.
| Orbit class | SSO |
| Inclination | 98.9159° |
| Eccentricity | 0.0001184 |
| Period | 101.1 min |
| Apogee | 812 km |
| Perigee | 810 km |
| Mean motion | 14.24371426 rev/day |
| RAAN | 175.7761° |
| Arg of perigee | 18.9574° |
| Mean anomaly | 341.1648° |
| B* | 4.3753e-5 |
| Rev at epoch | 36,414 |
1 44387U 19038A 26188.19454420 .00000055 00000-0 43753-4 0 99972 44387 98.9159 175.7761 0001184 18.9574 341.1648 14.24371426364140{
"OBJECT_NAME": "METEOR-M2 2",
"OBJECT_ID": "2019-038A",
"EPOCH": "2026-07-07T04:40:08.619+00:00",
"MEAN_MOTION": 14.24371426,
"ECCENTRICITY": 0.0001184,
"INCLINATION": 98.9159,
"RA_OF_ASC_NODE": 175.7761,
"ARG_OF_PERICENTER": 18.9574,
"MEAN_ANOMALY": 341.1648,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 44387,
"REV_AT_EPOCH": 36414,
"BSTAR": 0.000043753,
"MEAN_MOTION_DOT": 5.5e-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 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 |