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 data is extracted from the following two-line orbital elements,
1 25501U 98058A 19110.49632324 -.00000119 00000-0 00000+0 0 9999
2 25501 8.6255 31.0818 0014368 314.8632 246.7700 0.98178198 74212
| Epoch (UTC): | 20 April 2019 11:54:42 |
| Eccentricity: | 0.0014368 |
| inclination: | 8.6255° |
| perigee height: | 36322 km |
| apogee height: | 36445 km |
| right ascension of ascending node: | 31.0818° |
| argument of perigee: | 314.8632° |
| revolutions per day: | 0.98178198 |
| mean anomaly at epoch: | 246.7700° |
| orbit number at epoch: | 7421 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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