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 59069U 26145.51912507 +.00000000 +00000-0 +00000-0 0 00000
2 59069 0.0657 328.4713 0003744 67.6938 67.5103 1.00272820 08
| Epoch (UTC): | 25 May 2026 12:27:32 |
| Eccentricity: | 0.0003744 |
| inclination: | 0.0657° |
| perigee height: | 35771 km |
| apogee height: | 35802 km |
| right ascension of ascending node: | 328.4713° |
| argument of perigee: | 67.6938° |
| revolutions per day: | 1.00272820 |
| mean anomaly at epoch: | 67.5103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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