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 56801U 26145.37769338 +.00000000 +00000-0 +56751-4 0 00005
2 56801 69.9987 130.9778 0003703 268.8611 91.2123 14.98329656 01
| Epoch (UTC): | 25 May 2026 09:03:52 |
| Eccentricity: | 0.0003703 |
| inclination: | 69.9987° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 130.9778° |
| argument of perigee: | 268.8611° |
| revolutions per day: | 14.98329656 |
| mean anomaly at epoch: | 91.2123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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