HISAKI (SPRINT-A) is a payload in LEO orbit, operated by Institute of Space and Astronautical Sci, launched 2013.
| Orbit class | LEO |
| Inclination | 29.7190° |
| Eccentricity | 0.0136918 |
| Period | 106.2 min |
| Apogee | 1,154 km |
| Perigee | 950 km |
| Mean motion | 13.55546235 rev/day |
| RAAN | 118.8323° |
| Arg of perigee | 178.1912° |
| Mean anomaly | 181.9173° |
| B* | 4.7966e-5 |
| Rev at epoch | 63,412 |
1 39253U 13049A 26188.08752426 .00000102 00000-0 47966-4 0 99972 39253 29.7190 118.8323 0136918 178.1912 181.9173 13.55546235634120{
"OBJECT_NAME": "HISAKI (SPRINT-A)",
"OBJECT_ID": "2013-049A",
"EPOCH": "2026-07-07T02:06:02.096+00:00",
"MEAN_MOTION": 13.55546235,
"ECCENTRICITY": 0.0136918,
"INCLINATION": 29.719,
"RA_OF_ASC_NODE": 118.8323,
"ARG_OF_PERICENTER": 178.1912,
"MEAN_ANOMALY": 181.9173,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 39253,
"REV_AT_EPOCH": 63412,
"BSTAR": 0.000047966,
"MEAN_MOTION_DOT": 0.00000102,
"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 | HISAKI (SPRINT-A) |
| Operator | Institute of Space and Astronautical SciHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree |
| 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 |