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 56779U 26145.39856472 +.00000000 +00000-0 +74444-4 0 00006
2 56779 69.9988 131.0515 0003543 268.2596 91.8157 14.98320861 07
| Epoch (UTC): | 25 May 2026 09:33:55 |
| Eccentricity: | 0.0003543 |
| inclination: | 69.9988° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 131.0515° |
| argument of perigee: | 268.2596° |
| revolutions per day: | 14.98320861 |
| mean anomaly at epoch: | 91.8157° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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