SATELIOT_2 is a payload in SSO orbit, operated by Sateliot, launched 2024.
| Orbit class | SSO |
| Inclination | 97.6818° |
| Eccentricity | 0.0001902 |
| Period | 96.2 min |
| Apogee | 579 km |
| Perigee | 577 km |
| Mean motion | 14.96437548 rev/day |
| RAAN | 262.7457° |
| Arg of perigee | 87.5691° |
| Mean anomaly | 272.5748° |
| B* | 1.9989e-4 |
| Rev at epoch | 10,295 |
1 60534U 24149BU 26188.15381676 .00002210 00000-0 19989-3 0 99942 60534 97.6818 262.7457 0001902 87.5691 272.5748 14.96437548102953{
"OBJECT_NAME": "SATELIOT_2",
"OBJECT_ID": "2024-149BU",
"EPOCH": "2026-07-07T03:41:29.768+00:00",
"MEAN_MOTION": 14.96437548,
"ECCENTRICITY": 0.0001902,
"INCLINATION": 97.6818,
"RA_OF_ASC_NODE": 262.7457,
"ARG_OF_PERICENTER": 87.5691,
"MEAN_ANOMALY": 272.5748,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 60534,
"REV_AT_EPOCH": 10295,
"BSTAR": 0.00019989,
"MEAN_MOTION_DOT": 0.0000221,
"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 | SATELIOT_2 |
| Operator | |
| Country | Spain |
| 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 |