SENTINEL-2B is a payload in SSO orbit, operated by European Commission DG-GROW Directorate I/2, Copernicus Unit / European Space Agency, launched 2017.
| Orbit class | SSO |
| Inclination | 98.5681° |
| Eccentricity | 0.0001177 |
| Period | 100.6 min |
| Apogee | 790 km |
| Perigee | 788 km |
| Mean motion | 14.30813168 rev/day |
| RAAN | 262.6992° |
| Arg of perigee | 90.5457° |
| Mean anomaly | 269.5861° |
| B* | -2.7602e-5 |
| Rev at epoch | 48,750 |
1 42063U 17013A 26188.20749049 -.00000116 00000-0 -27602-4 0 99982 42063 98.5681 262.6992 0001177 90.5457 269.5861 14.30813168487502{
"OBJECT_NAME": "SENTINEL-2B",
"OBJECT_ID": "2017-013A",
"EPOCH": "2026-07-07T04:58:47.178+00:00",
"MEAN_MOTION": 14.30813168,
"ECCENTRICITY": 0.0001177,
"INCLINATION": 98.5681,
"RA_OF_ASC_NODE": 262.6992,
"ARG_OF_PERICENTER": 90.5457,
"MEAN_ANOMALY": 269.5861,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 42063,
"REV_AT_EPOCH": 48750,
"BSTAR": -0.000027602,
"MEAN_MOTION_DOT": -0.00000116,
"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 | SENTINEL-2B |
| Operator | European Commission DG-GROW Directorate I/2, Copernicus Unit / European Space AgencyHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree |
| Country | European Union |
| Launch date | |
| Launch mass (kg) |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Mission purpose | — |
| Object class |
| Orbital regime |
| Status |