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 59714U 26145.42220183 +.00000000 +00000-0 +27728-4 0 00009
2 59714 53.1587 308.0338 0001029 84.6086 275.5049 15.69714032 06
| Epoch (UTC): | 25 May 2026 10:07:58 |
| Eccentricity: | 0.0001029 |
| inclination: | 53.1587° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 308.0338° |
| argument of perigee: | 84.6086° |
| revolutions per day: | 15.69714032 |
| mean anomaly at epoch: | 275.5049° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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