MERIDIAN-M 21L is a payload in HEO orbit, operated by Aerospace Defence Forces, launched 2026.
Orbital data last updated 3 days ago. This may not reflect the current orbital state — not for operational use or collision avoidance.
| Orbit class | HEO |
| Inclination | 62.8109° |
| Eccentricity | 0.7167358 |
| Period | 717.8 min |
| Apogee | 39,211 km |
| Perigee | 1,144 km |
| Mean motion | 2.00615746 rev/day |
| RAAN | 226.4649° |
| Arg of perigee | 285.2786° |
| Mean anomaly | 11.3251° |
| B* | 0.0000e+0 |
| Rev at epoch | 185 |
1 68571U 26071A 26185.16055649 .00000159 00000-0 00000-0 0 99962 68571 62.8109 226.4649 7167358 285.2786 11.3251 2.00615746 1851{
"OBJECT_NAME": "MERIDIAN-M 21L",
"OBJECT_ID": "2026-071A",
"EPOCH": "2026-07-04T03:51:12.081+00:00",
"MEAN_MOTION": 2.00615746,
"ECCENTRICITY": 0.71673578,
"INCLINATION": 62.8109,
"RA_OF_ASC_NODE": 226.4649,
"ARG_OF_PERICENTER": 285.2786,
"MEAN_ANOMALY": 11.3251,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 68571,
"REV_AT_EPOCH": 185,
"BSTAR": 0,
"MEAN_MOTION_DOT": 0.00000159,
"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 | MERIDIAN-M 21L |
| 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 |