CE-SAT IIB is a payload in SSO orbit, operated by Canon Electronics Ltd., launched 2020.
| Orbit class | SSO |
| Inclination | 97.1852° |
| Eccentricity | 0.0005419 |
| Period | 89.0 min |
| Apogee | 228 km |
| Perigee | 221 km |
| Mean motion | 16.18332977 rev/day |
| RAAN | 272.6380° |
| Arg of perigee | 187.3834° |
| Mean anomaly | 172.7376° |
| B* | 4.8898e-4 |
| Rev at epoch | 31,847 |
1 46818U 20077F 26188.01626711 .00810436 22979-5 48898-3 0 99982 46818 97.1852 272.6380 0005419 187.3834 172.7376 16.18332977318475{
"OBJECT_NAME": "CE-SAT IIB",
"OBJECT_ID": "2020-077F",
"EPOCH": "2026-07-07T00:23:25.478+00:00",
"MEAN_MOTION": 16.18332977,
"ECCENTRICITY": 0.0005419,
"INCLINATION": 97.1852,
"RA_OF_ASC_NODE": 272.638,
"ARG_OF_PERICENTER": 187.3834,
"MEAN_ANOMALY": 172.7376,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 46818,
"REV_AT_EPOCH": 31847,
"BSTAR": 0.00048898,
"MEAN_MOTION_DOT": 0.00810436,
"MEAN_MOTION_DDOT": 0.0000022979
}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 | CE-SAT IIB |
| Operator | |
| Country | Japan |
| Launch date | |
| Launch mass (kg) | |
| Mission purpose | — |
| Object class |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Orbital regime |
| Status |