2025-313B is a payload in SSO orbit, operated by NPO Applied Mechanics / Moscow Aviation Institute, Student KB Iskra, launched 2025.
| Orbit class | SSO |
| Inclination | 97.5106° |
| Eccentricity | 0.0290775 |
| Period | 97.7 min |
| Apogee | 852 km |
| Perigee | 443 km |
| Mean motion | 14.74330925 rev/day |
| RAAN | 251.9818° |
| Arg of perigee | 270.8938° |
| Mean anomaly | 85.8971° |
| B* | 1.0997e-4 |
| Rev at epoch | 2,805 |
1 67249U 25313B 26187.98572160 .00001376 00000-0 10997-3 0 99902 67249 97.5106 251.9818 0290775 270.8938 85.8971 14.74330925 28050{
"OBJECT_NAME": "2025-313B",
"OBJECT_ID": "2025-313B",
"EPOCH": "2026-07-06T23:39:26.346+00:00",
"MEAN_MOTION": 14.74330925,
"ECCENTRICITY": 0.0290775,
"INCLINATION": 97.5106,
"RA_OF_ASC_NODE": 251.9818,
"ARG_OF_PERICENTER": 270.8938,
"MEAN_ANOMALY": 85.8971,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 67249,
"REV_AT_EPOCH": 2805,
"BSTAR": 0.00010997,
"MEAN_MOTION_DOT": 0.00001376,
"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 | 2025-313B |
| Operator | NPO Applied Mechanics / Moscow Aviation Institute, Student KB IskraHIGHvia 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 |