NUSAT-52 is a payload in SSO orbit, operated by URUGUS S.A., Satellogic S.A., Montevideo satellite factory, launched 2025.
| Orbit class | SSO |
| Inclination | 97.4197° |
| Eccentricity | 0.0001977 |
| Period | 94.7 min |
| Apogee | 507 km |
| Perigee | 505 km |
| Mean motion | 15.19985034 rev/day |
| RAAN | 261.3805° |
| Arg of perigee | 330.8162° |
| Mean anomaly | 29.2962° |
| B* | 1.9327e-4 |
| Rev at epoch | 3,345 |
1 66692U 25276AC 26188.16260259 .00004093 00000-0 19327-3 0 99982 66692 97.4197 261.3805 0001977 330.8162 29.2962 15.19985034 33450{
"OBJECT_NAME": "NUSAT-52",
"OBJECT_ID": "2025-276AC",
"EPOCH": "2026-07-07T03:54:08.864+00:00",
"MEAN_MOTION": 15.19985034,
"ECCENTRICITY": 0.0001977,
"INCLINATION": 97.4197,
"RA_OF_ASC_NODE": 261.3805,
"ARG_OF_PERICENTER": 330.8162,
"MEAN_ANOMALY": 29.2962,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 66692,
"REV_AT_EPOCH": 3345,
"BSTAR": 0.00019327,
"MEAN_MOTION_DOT": 0.00004093,
"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-52 |
| 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 |