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 57778U 26145.34135859 +.00000000 +00000-0 +17949-4 0 00007
2 57778 43.0042 110.1094 0001173 270.1105 89.9612 15.27573338 02
| Epoch (UTC): | 25 May 2026 08:11:33 |
| Eccentricity: | 0.0001173 |
| inclination: | 43.0042° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 110.1094° |
| argument of perigee: | 270.1105° |
| revolutions per day: | 15.27573338 |
| mean anomaly at epoch: | 89.9612° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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