NUSAT-40 (C SHOEMAKER) is a payload in SSO orbit, operated by URUGUS S.A., Satellogic S.A., Montevideo satellite factory, launched 2023.
| Orbit class | SSO |
| Inclination | 97.4859° |
| Eccentricity | 0.0004511 |
| Period | 91.1 min |
| Apogee | 332 km |
| Perigee | 325 km |
| Mean motion | 15.80697836 rev/day |
| RAAN | 336.3478° |
| Arg of perigee | 200.9611° |
| Mean anomaly | 159.1472° |
| B* | 5.7150e-4 |
| Rev at epoch | 17,196 |
1 56943U 23084M 26188.18835155 .00110186 00000-0 57150-3 0 99932 56943 97.4859 336.3478 0004511 200.9611 159.1472 15.80697836171961{
"OBJECT_NAME": "NUSAT-40 (C SHOEMAKER)",
"OBJECT_ID": "2023-084M",
"EPOCH": "2026-07-07T04:31:13.574+00:00",
"MEAN_MOTION": 15.80697836,
"ECCENTRICITY": 0.0004511,
"INCLINATION": 97.4859,
"RA_OF_ASC_NODE": 336.3478,
"ARG_OF_PERICENTER": 200.9611,
"MEAN_ANOMALY": 159.1472,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 56943,
"REV_AT_EPOCH": 17196,
"BSTAR": 0.0005715,
"MEAN_MOTION_DOT": 0.00110186,
"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-40 (C SHOEMAKER) |
| 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 |