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 59579U 26145.43623233 +.00000000 +00000-0 +67096-4 0 00004
2 59579 43.0015 295.2630 0001152 272.9291 87.1429 15.27578687 05
| Epoch (UTC): | 25 May 2026 10:28:10 |
| Eccentricity: | 0.0001152 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 295.2630° |
| argument of perigee: | 272.9291° |
| revolutions per day: | 15.27578687 |
| mean anomaly at epoch: | 87.1429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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