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 66359U 26145.50880139 +.00000000 +00000-0 +58722-3 0 00001
2 66359 53.1604 235.1651 0001724 99.5442 260.5755 15.31721453 02
| Epoch (UTC): | 25 May 2026 12:12:40 |
| Eccentricity: | 0.0001724 |
| inclination: | 53.1604° |
| perigee height: | 469 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 235.1651° |
| argument of perigee: | 99.5442° |
| revolutions per day: | 15.31721453 |
| mean anomaly at epoch: | 260.5755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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