ICEYE-X26 is a payload in SSO orbit, operated by ICEYE US, launched 2023.
Orbital data last updated 45 days ago. This may not reflect the current orbital state — not for operational use or collision avoidance.
| Orbit class | SSO |
| Inclination | 97.5706° |
| Eccentricity | 0.0008963 |
| Period | 89.9 min |
| Apogee | 277 km |
| Perigee | 265 km |
| Mean motion | 16.01192802 rev/day |
| RAAN | 305.8425° |
| Arg of perigee | 278.0989° |
| Mean anomaly | 81.9272° |
| B* | 1.3206e-3 |
| Rev at epoch | 16,520 |
1 56961U 23084AF 26142.63340083 .00716713 24170-3 13206-2 0 99922 56961 97.5706 305.8425 0008963 278.0989 81.9272 16.01192802165202{
"OBJECT_NAME": "ICEYE-X26",
"OBJECT_ID": "2023-084AF",
"EPOCH": "2026-05-22T15:12:05.832+00:00",
"MEAN_MOTION": 16.01192802,
"ECCENTRICITY": 0.0008963,
"INCLINATION": 97.5706,
"RA_OF_ASC_NODE": 305.8425,
"ARG_OF_PERICENTER": 278.0989,
"MEAN_ANOMALY": 81.9272,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 56961,
"REV_AT_EPOCH": 16520,
"BSTAR": 0.0013206,
"MEAN_MOTION_DOT": 0.00716713,
"MEAN_MOTION_DDOT": 0.0002417
}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 | ICEYE-X26 |
| Operator | |
| Country | United States |
| 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 |