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 59337U 26145.61534889 +.00000000 +00000-0 +69059-5 0 00006
2 59337 43.0019 112.6572 0000851 274.3086 85.7668 15.27573650 05
| Epoch (UTC): | 25 May 2026 14:46:06 |
| Eccentricity: | 0.0000851 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 112.6572° |
| argument of perigee: | 274.3086° |
| revolutions per day: | 15.27573650 |
| mean anomaly at epoch: | 85.7668° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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