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 59179U 26145.34766747 +.00000000 +00000-0 +33078-3 0 00000
2 59179 43.0017 19.7600 0000767 292.7596 67.3175 15.27579141 02
| Epoch (UTC): | 25 May 2026 08:20:38 |
| Eccentricity: | 0.0000767 |
| inclination: | 43.0017° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 19.7600° |
| argument of perigee: | 292.7596° |
| revolutions per day: | 15.27579141 |
| mean anomaly at epoch: | 67.3175° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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