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 07659U 26088.16563440 +.00000000 +00000-0 +29749-3 0 00007
2 07659 49.8147 49.5655 0185023 64.1626 297.8227 13.94040631 08
| Epoch (UTC): | 29 March 2026 03:58:30 |
| Eccentricity: | 0.0185023 |
| inclination: | 49.8147° |
| perigee height: | 780 km |
| apogee height: | 1049 km |
| right ascension of ascending node: | 49.5655° |
| argument of perigee: | 64.1626° |
| revolutions per day: | 13.94040631 |
| mean anomaly at epoch: | 297.8227° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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