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 59780U 26145.58369854 +.00000000 +00000-0 +67398-4 0 00005
2 59780 98.6672 264.6442 0011070 276.4122 83.5800 14.31836157 03
| Epoch (UTC): | 25 May 2026 14:00:31 |
| Eccentricity: | 0.0011070 |
| inclination: | 98.6672° |
| perigee height: | 778 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 264.6442° |
| argument of perigee: | 276.4122° |
| revolutions per day: | 14.31836157 |
| mean anomaly at epoch: | 83.5800° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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