TIRSAT is a payload in SSO orbit, operated by Japan Space Systems, launched 2024.
| Orbit class | SSO |
| Inclination | 97.9961° |
| Eccentricity | 0.0006335 |
| Period | 97.8 min |
| Apogee | 658 km |
| Perigee | 649 km |
| Mean motion | 14.72508195 rev/day |
| RAAN | 245.4395° |
| Arg of perigee | 89.0247° |
| Mean anomaly | 271.1686° |
| B* | 2.0004e-4 |
| Rev at epoch | 12,791 |
1 58989U 24032C 26187.40649191 .00001221 00000-0 20004-3 0 99932 58989 97.9961 245.4395 0006336 89.0247 271.1686 14.72508195127915{
"OBJECT_NAME": "TIRSAT",
"OBJECT_ID": "2024-032C",
"EPOCH": "2026-07-06T09:45:20.901+00:00",
"MEAN_MOTION": 14.72508195,
"ECCENTRICITY": 0.00063355,
"INCLINATION": 97.9961,
"RA_OF_ASC_NODE": 245.4395,
"ARG_OF_PERICENTER": 89.0247,
"MEAN_ANOMALY": 271.1686,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 58989,
"REV_AT_EPOCH": 12791,
"BSTAR": 0.00020003778,
"MEAN_MOTION_DOT": 0.00001221,
"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 | TIRSAT |
| 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 |