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 58755U 26145.62529299 +.00000000 +00000-0 +17179-3 0 00003
2 58755 97.5271 213.4169 0012975 30.1478 330.0496 15.12108547 05
| Epoch (UTC): | 25 May 2026 15:00:25 |
| Eccentricity: | 0.0012975 |
| inclination: | 97.5271° |
| perigee height: | 521 km |
| apogee height: | 539 km |
| right ascension of ascending node: | 213.4169° |
| argument of perigee: | 30.1478° |
| revolutions per day: | 15.12108547 |
| mean anomaly at epoch: | 330.0496° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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