NUSAT-50 (NANCY ROMAN) is a payload in SSO orbit, operated by URUGUS S.A., Satellogic S.A., Montevideo satellite factory, launched 2024.
| Orbit class | SSO |
| Inclination | 97.3778° |
| Eccentricity | 0.0004730 |
| Period | 94.1 min |
| Apogee | 478 km |
| Perigee | 472 km |
| Mean motion | 15.30223041 rev/day |
| RAAN | 269.3014° |
| Arg of perigee | 121.0108° |
| Mean anomaly | 239.1598° |
| B* | 2.4510e-4 |
| Rev at epoch | 10,518 |
1 60493U 24149AB 26188.18099550 .00007093 00000-0 24510-3 0 99982 60493 97.3778 269.3014 0004730 121.0108 239.1598 15.30223041105180{
"OBJECT_NAME": "NUSAT-50 (NANCY ROMAN)",
"OBJECT_ID": "2024-149AB",
"EPOCH": "2026-07-07T04:20:38.011+00:00",
"MEAN_MOTION": 15.30223041,
"ECCENTRICITY": 0.000473,
"INCLINATION": 97.3778,
"RA_OF_ASC_NODE": 269.3014,
"ARG_OF_PERICENTER": 121.0108,
"MEAN_ANOMALY": 239.1598,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 60493,
"REV_AT_EPOCH": 10518,
"BSTAR": 0.0002451,
"MEAN_MOTION_DOT": 0.00007093,
"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-50 (NANCY ROMAN) |
| 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 |