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 26546U 00057B 18110.96205656 +.00000101 +00000-0 +26057-4 0 9991
2 26546 064.5536 091.8541 0008220 308.4463 051.5909 14.90711339952511
| Epoch (UTC): | 20 April 2018 23:05:21 |
| Eccentricity: | 0.0008220 |
| inclination: | 64.5536° |
| perigee height: | 590 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 91.8541° |
| argument of perigee: | 308.4463° |
| revolutions per day: | 14.90711339 |
| mean anomaly at epoch: | 51.5909° |
| orbit number at epoch: | 95251 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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