JCSAT-16 is a payload in GEO orbit, operated by Sky Perfect JSAT Corp., launched 2016.
| Orbit class | GEO |
| Inclination | 0.0198° |
| Eccentricity | 0.0000983 |
| Period | 1436.1 min |
| Apogee | 35,791 km |
| Perigee | 35,783 km |
| Mean motion | 1.00269925 rev/day |
| RAAN | 41.5076° |
| Arg of perigee | 73.1913° |
| Mean anomaly | 16.5553° |
| B* | 0.0000e+0 |
| Rev at epoch | 3,627 |
1 41729U 16050A 26188.17266956 -.00000236 00000-0 00000-0 0 99942 41729 0.0198 41.5076 0000983 73.1913 16.5553 1.00269925 36277{
"OBJECT_NAME": "JCSAT-16",
"OBJECT_ID": "2016-050A",
"EPOCH": "2026-07-07T04:08:38.65+00:00",
"MEAN_MOTION": 1.00269925,
"ECCENTRICITY": 0.0000983,
"INCLINATION": 0.0198,
"RA_OF_ASC_NODE": 41.5076,
"ARG_OF_PERICENTER": 73.1913,
"MEAN_ANOMALY": 16.5553,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 41729,
"REV_AT_EPOCH": 3627,
"BSTAR": 0,
"MEAN_MOTION_DOT": -0.00000236,
"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 | JCSAT-16 |
| Operator | |
| Country | Japan |
| Launch date | |
| Launch mass (kg) | |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Mission purpose |
| — |
| Object class |
| Orbital regime |
| Status |