AAC-HSI-SAT2 is a payload in SSO orbit, operated by AAC Microtec/Clyde Space Ltd. / Wyvern Inc., launched 2023.
| Orbit class | SSO |
| Inclination | 97.8279° |
| Eccentricity | 0.0013569 |
| Period | 94.7 min |
| Apogee | 513 km |
| Perigee | 495 km |
| Mean motion | 15.20592143 rev/day |
| RAAN | 339.2206° |
| Arg of perigee | 114.2164° |
| Mean anomaly | 246.0489° |
| B* | 2.4973e-4 |
| Rev at epoch | 16,938 |
1 56995U 23084BX 26188.21928021 .00005410 00000-0 24973-3 0 99992 56995 97.8279 339.2206 0013569 114.2164 246.0489 15.20592143169388{
"OBJECT_NAME": "AAC-HSI-SAT2",
"OBJECT_ID": "2023-084BX",
"EPOCH": "2026-07-07T05:15:45.81+00:00",
"MEAN_MOTION": 15.20592143,
"ECCENTRICITY": 0.0013569,
"INCLINATION": 97.8279,
"RA_OF_ASC_NODE": 339.2206,
"ARG_OF_PERICENTER": 114.2164,
"MEAN_ANOMALY": 246.0489,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 56995,
"REV_AT_EPOCH": 16938,
"BSTAR": 0.00024973,
"MEAN_MOTION_DOT": 0.0000541,
"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 | AAC-HSI-SAT2 |
| Operator | AAC Microtec/Clyde Space Ltd. / Wyvern Inc.HIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree |
| Country | |
| Launch date | |
| Launch mass (kg) | 10HIGH |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Mission purpose | — |
| Object class |
| Orbital regime |
| Status |