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 56795U 26145.36950698 +.00000000 +00000-0 +32303-4 0 00004
2 56795 69.9987 130.9489 0003777 265.7658 94.3069 14.98332260 08
| Epoch (UTC): | 25 May 2026 08:52:05 |
| Eccentricity: | 0.0003777 |
| inclination: | 69.9987° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 130.9489° |
| argument of perigee: | 265.7658° |
| revolutions per day: | 14.98332260 |
| mean anomaly at epoch: | 94.3069° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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