NUSAT-26 (M SOMERVILLE) is a payload in SSO orbit, operated by URUGUS S.A., Satellogic S.A., Montevideo satellite factory, launched 2022.
| Orbit class | SSO |
| Inclination | 97.2337° |
| Eccentricity | 0.0006498 |
| Period | 93.3 min |
| Apogee | 442 km |
| Perigee | 433 km |
| Mean motion | 15.43032390 rev/day |
| RAAN | 267.0909° |
| Arg of perigee | 162.6896° |
| Mean anomaly | 197.4574° |
| B* | 3.5031e-4 |
| Rev at epoch | 10,778 |
1 52184U 22033AD 26188.15673198 .00015392 00000-0 35031-3 0 99902 52184 97.2337 267.0909 0006498 162.6896 197.4574 15.43032390107781{
"OBJECT_NAME": "NUSAT-26 (M SOMERVILLE)",
"OBJECT_ID": "2022-033AD",
"EPOCH": "2026-07-07T03:45:41.643+00:00",
"MEAN_MOTION": 15.4303239,
"ECCENTRICITY": 0.0006498,
"INCLINATION": 97.2337,
"RA_OF_ASC_NODE": 267.0909,
"ARG_OF_PERICENTER": 162.6896,
"MEAN_ANOMALY": 197.4574,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 52184,
"REV_AT_EPOCH": 10778,
"BSTAR": 0.00035031,
"MEAN_MOTION_DOT": 0.00015392,
"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 | NUSAT-26 (M SOMERVILLE) |
| Operator | URUGUS S.A., Satellogic S.A., Montevideo satellite factoryHIGHvia GCAT — Jonathan McDowell's General Catalog |
| Country | UY |
| 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 |