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 59699U 26145.58376748 +.00000000 +00000-0 +27585-3 0 00007
2 59699 43.0000 345.5092 0000869 267.2005 92.8747 15.27598487 03
| Epoch (UTC): | 25 May 2026 14:00:37 |
| Eccentricity: | 0.0000869 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 345.5092° |
| argument of perigee: | 267.2005° |
| revolutions per day: | 15.27598487 |
| mean anomaly at epoch: | 92.8747° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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