IRIDE-MS1-EAGLET 2-10 is a payload in SSO orbit, operated by Italian Space Agency / OHB-I (Compagnia Generale per lo Spazio), launched 2026.
| Orbit class | SSO |
| Inclination | 97.4514° |
| Eccentricity | 0.0001397 |
| Period | 94.8 min |
| Apogee | 509 km |
| Perigee | 507 km |
| Mean motion | 15.19154646 rev/day |
| RAAN | 146.0806° |
| Arg of perigee | 51.0155° |
| Mean anomaly | 309.1204° |
| B* | 2.2271e-4 |
| Rev at epoch | 1,493 |
1 68451U 26067AM 26187.88619616 .00004613 00000-0 22271-3 0 99952 68451 97.4514 146.0806 0001397 51.0155 309.1204 15.19154646 14936{
"OBJECT_NAME": "IRIDE-MS1-EAGLET 2-10",
"OBJECT_ID": "2026-067AM",
"EPOCH": "2026-07-06T21:16:07.348+00:00",
"MEAN_MOTION": 15.19154646,
"ECCENTRICITY": 0.0001397,
"INCLINATION": 97.4514,
"RA_OF_ASC_NODE": 146.0806,
"ARG_OF_PERICENTER": 51.0155,
"MEAN_ANOMALY": 309.1204,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 68451,
"REV_AT_EPOCH": 1493,
"BSTAR": 0.00022271,
"MEAN_MOTION_DOT": 0.00004613,
"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 | IRIDE-MS1-EAGLET 2-10 |
| Operator | Italian Space Agency / OHB-I (Compagnia Generale per lo Spazio)HIGHvia GCAT — Jonathan McDowell's General Catalog |
| Country | Italy |
| 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 |