OPTICUBE 04 is a payload in SSO orbit, operated by US Air Force Research Laboratories/RV (Space Vehicles Directorate) / California Polytechnic State University, launched 2016.
| Orbit class | SSO |
| Inclination | 98.0683° |
| Eccentricity | 0.0016763 |
| Period | 95.4 min |
| Apogee | 549 km |
| Perigee | 525 km |
| Mean motion | 15.09746613 rev/day |
| RAAN | 40.8590° |
| Arg of perigee | 55.4583° |
| Mean anomaly | 304.8224° |
| B* | 1.2097e-4 |
| Rev at epoch | 52,809 |
1 41851U 16067D 26187.56538133 .00001886 00000-0 12097-3 0 99922 41851 98.0683 40.8590 0016763 55.4583 304.8224 15.09746613528093{
"OBJECT_NAME": "OPTICUBE 04",
"OBJECT_ID": "2016-067D",
"EPOCH": "2026-07-06T13:34:08.947+00:00",
"MEAN_MOTION": 15.09746613,
"ECCENTRICITY": 0.0016763,
"INCLINATION": 98.0683,
"RA_OF_ASC_NODE": 40.859,
"ARG_OF_PERICENTER": 55.4583,
"MEAN_ANOMALY": 304.8224,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 41851,
"REV_AT_EPOCH": 52809,
"BSTAR": 0.00012097,
"MEAN_MOTION_DOT": 0.00001886,
"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 | OPTICUBE 04 |
| Operator | US Air Force Research Laboratories/RV (Space Vehicles Directorate) / California Polytechnic State UniversityHIGHvia 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 |