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 57773U 26145.34212100 +.00000000 +00000-0 +90332-4 0 00004
2 57773 43.0035 124.6805 0001631 288.8633 71.2042 15.27584597 00
| Epoch (UTC): | 25 May 2026 08:12:39 |
| Eccentricity: | 0.0001631 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 124.6805° |
| argument of perigee: | 288.8633° |
| revolutions per day: | 15.27584597 |
| mean anomaly at epoch: | 71.2042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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