MULE 4T is a payload in SSO orbit, operated by Experimental and Design Bureau (OKB) Fifth Generation, launched 2025.
| Orbit class | SSO |
| Inclination | 97.3925° |
| Eccentricity | 0.0007945 |
| Period | 94.5 min |
| Apogee | 498 km |
| Perigee | 487 km |
| Mean motion | 15.24550129 rev/day |
| RAAN | 262.3734° |
| Arg of perigee | 286.7445° |
| Mean anomaly | 73.2920° |
| B* | 2.6534e-4 |
| Rev at epoch | 2,894 |
1 67286U 25313AQ 26187.70142544 .00006467 00000-0 26534-3 0 99902 67286 97.3925 262.3734 0007945 286.7445 73.2920 15.24550129 28944{
"OBJECT_NAME": "MULE 4T",
"OBJECT_ID": "2025-313AQ",
"EPOCH": "2026-07-06T16:50:03.158+00:00",
"MEAN_MOTION": 15.24550129,
"ECCENTRICITY": 0.0007945,
"INCLINATION": 97.3925,
"RA_OF_ASC_NODE": 262.3734,
"ARG_OF_PERICENTER": 286.7445,
"MEAN_ANOMALY": 73.292,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 67286,
"REV_AT_EPOCH": 2894,
"BSTAR": 0.00026534,
"MEAN_MOTION_DOT": 0.00006467,
"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 | MULE 4T |
| Operator | Experimental and Design Bureau (OKB) Fifth GenerationHIGHvia 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 |