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 59588U 26109.07970916 +.00000000 +00000-0 +19457-1 0 00002
2 59588 97.1863 41.1236 0069452 354.8334 5.2106 13.91597884 03
| Epoch (UTC): | 19 April 2026 01:54:46 |
| Eccentricity: | 0.0069452 |
| inclination: | 97.1863° |
| perigee height: | 872 km |
| apogee height: | 974 km |
| right ascension of ascending node: | 41.1236° |
| argument of perigee: | 354.8334° |
| revolutions per day: | 13.91597884 |
| mean anomaly at epoch: | 5.2106° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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