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 41915U 17002C 19111.84007252 .00000259 00000-0 19142-4 0 9998
2 41915 97.4453 181.9502 0008804 309.6462 143.5834 15.11285664125724
| Epoch (UTC): | 21 April 2019 20:09:42 |
| Eccentricity: | 0.0008804 |
| inclination: | 97.4453° |
| perigee height: | 526 km |
| apogee height: | 538 km |
| right ascension of ascending node: | 181.9502° |
| argument of perigee: | 309.6462° |
| revolutions per day: | 15.11285664 |
| mean anomaly at epoch: | 143.5834° |
| orbit number at epoch: | 12572 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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