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 26093U 00004L 19082.91588050 +.00000170 +00000-0 +58159-4 0 9990
2 26093 100.1886 335.8267 0030633 345.2915 014.7379 14.51566202008320
| Epoch (UTC): | 23 March 2019 21:58:52 |
| Eccentricity: | 0.0030633 |
| inclination: | 100.1886° |
| perigee height: | 699 km |
| apogee height: | 742 km |
| right ascension of ascending node: | 335.8267° |
| argument of perigee: | 345.2915° |
| revolutions per day: | 14.51566202 |
| mean anomaly at epoch: | 14.7379° |
| orbit number at epoch: | 832 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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