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 59575U 26145.13932947 +.00000000 +00000-0 -11959-3 0 00009
2 59575 43.0036 293.8942 0002936 284.5188 75.5338 15.27597726 04
| Epoch (UTC): | 25 May 2026 03:20:38 |
| Eccentricity: | 0.0002936 |
| inclination: | 43.0036° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 293.8942° |
| argument of perigee: | 284.5188° |
| revolutions per day: | 15.27597726 |
| mean anomaly at epoch: | 75.5338° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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