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 59728U 26145.79257763 +.00000000 +00000-0 +65891-4 0 00001
2 59728 97.7766 148.0348 0001836 270.5054 89.5952 14.87001264 05
| Epoch (UTC): | 25 May 2026 19:01:18 |
| Eccentricity: | 0.0001836 |
| inclination: | 97.7766° |
| perigee height: | 606 km |
| apogee height: | 609 km |
| right ascension of ascending node: | 148.0348° |
| argument of perigee: | 270.5054° |
| revolutions per day: | 14.87001264 |
| mean anomaly at epoch: | 89.5952° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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