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 59797U 26145.44467759 +.00000000 +00000-0 +42727-4 0 00000
2 59797 43.0017 135.4602 0001116 267.6053 92.4671 15.27577500 01
| Epoch (UTC): | 25 May 2026 10:40:20 |
| Eccentricity: | 0.0001116 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 135.4602° |
| argument of perigee: | 267.6053° |
| revolutions per day: | 15.27577500 |
| mean anomaly at epoch: | 92.4671° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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