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 56778U 26145.35684786 +.00000000 +00000-0 +62141-5 0 00000
2 56778 69.9987 131.3083 0003568 267.7270 92.3480 14.98331529 06
| Epoch (UTC): | 25 May 2026 08:33:51 |
| Eccentricity: | 0.0003568 |
| inclination: | 69.9987° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 131.3083° |
| argument of perigee: | 267.7270° |
| revolutions per day: | 14.98331529 |
| mean anomaly at epoch: | 92.3480° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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