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 59568U 26145.12215068 +.00000000 +00000-0 +15894-4 0 00000
2 59568 43.0015 297.2094 0000847 288.6526 71.4234 15.27579197 01
| Epoch (UTC): | 25 May 2026 02:55:53 |
| Eccentricity: | 0.0000847 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 297.2094° |
| argument of perigee: | 288.6526° |
| revolutions per day: | 15.27579197 |
| mean anomaly at epoch: | 71.4234° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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