View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 66059U 26145.57939517 +.00000000 +00000-0 +31153-3 0 00009
2 66059 53.1568 248.1241 0000348 13.1117 346.9893 15.30198630 05
| Epoch (UTC): | 25 May 2026 13:54:19 |
| Eccentricity: | 0.0000348 |
| inclination: | 53.1568° |
| perigee height: | 475 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 248.1241° |
| argument of perigee: | 13.1117° |
| revolutions per day: | 15.30198630 |
| mean anomaly at epoch: | 346.9893° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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