AC1-003 is a payload in SSO orbit, operated by BAE Systems Digital Intelligence (Detica) / BAE In-Space Missions, launched 2025.
| Orbit class | SSO |
| Inclination | 97.4195° |
| Eccentricity | 0.0001581 |
| Period | 94.8 min |
| Apogee | 512 km |
| Perigee | 510 km |
| Mean motion | 15.18314683 rev/day |
| RAAN | 261.0748° |
| Arg of perigee | 334.6839° |
| Mean anomaly | 25.4318° |
| B* | 1.0146e-4 |
| Rev at epoch | 3,343 |
1 66689U 25276Z 26188.15751160 .00002014 00000-0 10146-3 0 99902 66689 97.4195 261.0748 0001581 334.6839 25.4318 15.18314683 33437{
"OBJECT_NAME": "AC1-003",
"OBJECT_ID": "2025-276Z",
"EPOCH": "2026-07-07T03:46:49.002+00:00",
"MEAN_MOTION": 15.18314683,
"ECCENTRICITY": 0.0001581,
"INCLINATION": 97.4195,
"RA_OF_ASC_NODE": 261.0748,
"ARG_OF_PERICENTER": 334.6839,
"MEAN_ANOMALY": 25.4318,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 66689,
"REV_AT_EPOCH": 3343,
"BSTAR": 0.00010146,
"MEAN_MOTION_DOT": 0.00002014,
"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 | AC1-003 |
| Operator | BAE Systems Digital Intelligence (Detica) / BAE In-Space MissionsHIGHvia GCAT — Jonathan McDowell's General Catalog |
| Country | United Kingdom |
| Launch date | |
| Launch mass (kg) | |
| Mission purpose | — |
| Object class | PAYLOADHIGH |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Orbital regime |
| Status |