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 18181.58735826 0.00000000 00000-0 00000-0 0 09
2 25501 8.3658 32.2154 0013996 315.6559 44.2442 0.98177708 01
| Epoch (UTC): | 30 June 2018 14:05:47 |
| Eccentricity: | 0.0013996 |
| inclination: | 8.3658° |
| perigee height: | 36324 km |
| apogee height: | 36443 km |
| right ascension of ascending node: | 32.2154° |
| argument of perigee: | 315.6559° |
| revolutions per day: | 0.98177708 |
| mean anomaly at epoch: | 44.2442° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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