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 59854U 26145.51861500 +.00000000 +00000-0 -41961-4 0 00004
2 59854 42.9987 200.7417 0001035 284.1561 75.9176 15.27582014 09
| Epoch (UTC): | 25 May 2026 12:26:48 |
| Eccentricity: | 0.0001035 |
| inclination: | 42.9987° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.7417° |
| argument of perigee: | 284.1561° |
| revolutions per day: | 15.27582014 |
| mean anomaly at epoch: | 75.9176° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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