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 15595U 85021A 21021.53515683 -.00000066 00000-0 22751-4 0 9997
2 15595 108.0356 301.7284 0002701 271.0746 89.0086 14.38184247879324
| Epoch (UTC): | 21 January 2021 12:50:37 |
| Eccentricity: | 0.0002701 |
| inclination: | 108.0356° |
| perigee height: | 762 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 301.7284° |
| argument of perigee: | 271.0746° |
| revolutions per day: | 14.38184247 |
| mean anomaly at epoch: | 89.0086° |
| orbit number at epoch: | 87932 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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