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 65588U 26145.39219729 +.00000000 +00000-0 +00000-0 0 00005
2 65588 0.0127 80.0302 0000441 16.9086 40.0937 1.00268491 00
| Epoch (UTC): | 25 May 2026 09:24:45 |
| Eccentricity: | 0.0000441 |
| inclination: | 0.0127° |
| perigee height: | 35786 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 80.0302° |
| argument of perigee: | 16.9086° |
| revolutions per day: | 1.00268491 |
| mean anomaly at epoch: | 40.0937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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