RROCI-2 is a payload in SSO orbit, operated by US Space Force Space Systems Command / Orion Space Solutions, launched 2024.
| Orbit class | SSO |
| Inclination | 97.8549° |
| Eccentricity | 0.0009969 |
| Period | 96.0 min |
| Apogee | 574 km |
| Perigee | 560 km |
| Mean motion | 15.00046752 rev/day |
| RAAN | 320.9255° |
| Arg of perigee | 319.0692° |
| Mean anomaly | 40.9782° |
| B* | 1.7062e-4 |
| Rev at epoch | 12,773 |
1 59106U 24043J 26187.99874064 .00002064 00000-0 17062-3 0 99962 59106 97.8549 320.9255 0009969 319.0692 40.9782 15.00046752127734{
"OBJECT_NAME": "RROCI-2",
"OBJECT_ID": "2024-043J",
"EPOCH": "2026-07-06T23:58:11.191+00:00",
"MEAN_MOTION": 15.00046752,
"ECCENTRICITY": 0.0009969,
"INCLINATION": 97.8549,
"RA_OF_ASC_NODE": 320.9255,
"ARG_OF_PERICENTER": 319.0692,
"MEAN_ANOMALY": 40.9782,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 59106,
"REV_AT_EPOCH": 12773,
"BSTAR": 0.00017062,
"MEAN_MOTION_DOT": 0.00002064,
"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 | RROCI-2 |
| Operator | US Space Force Space Systems Command / Orion Space SolutionsHIGHvia GCAT — Jonathan McDowell's General Catalog |
| Country | United States |
| 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 |