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 53178U 26145.38894638 +.00000000 +00000-0 +56395-4 0 00006
2 53178 53.2114 179.8033 0000760 87.6191 272.4888 15.08835300 00
| Epoch (UTC): | 25 May 2026 09:20:04 |
| Eccentricity: | 0.0000760 |
| inclination: | 53.2114° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 179.8033° |
| argument of perigee: | 87.6191° |
| revolutions per day: | 15.08835300 |
| mean anomaly at epoch: | 272.4888° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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