QZS-1R (MICHIBIKI-1R) is a payload in MEO orbit, operated by Cabinet Space Strategy Office / Japan Aerospace Exploration Agency, launched 2021.
| Orbit class | MEO |
| Inclination | 37.4964° |
| Eccentricity | 0.0755511 |
| Period | 1436.4 min |
| Apogee | 38,979 km |
| Perigee | 32,607 km |
| Mean motion | 1.00249302 rev/day |
| RAAN | 79.3119° |
| Arg of perigee | 272.0883° |
| Mean anomaly | 281.1819° |
| B* | 0.0000e+0 |
| Rev at epoch | 1,719 |
1 49336U 21096A 26186.60108073 -.00000258 00000-0 00000-0 0 99972 49336 37.4964 79.3119 0755511 272.0883 281.1819 1.00249302 17193{
"OBJECT_NAME": "QZS-1R (MICHIBIKI-1R)",
"OBJECT_ID": "2021-096A",
"EPOCH": "2026-07-05T14:25:33.375+00:00",
"MEAN_MOTION": 1.00249302,
"ECCENTRICITY": 0.07555114,
"INCLINATION": 37.4964,
"RA_OF_ASC_NODE": 79.3119,
"ARG_OF_PERICENTER": 272.0883,
"MEAN_ANOMALY": 281.1819,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 49336,
"REV_AT_EPOCH": 1719,
"BSTAR": 0,
"MEAN_MOTION_DOT": -0.00000258,
"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 | QZS-1R (MICHIBIKI-1R) |
| Operator | Cabinet Space Strategy Office / Japan Aerospace Exploration AgencyHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree |
| Country | |
| Launch date | |
| Launch mass (kg) | 4020 |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Mission purpose | — |
| Object class |
| Orbital regime |
| Status |