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 29522U 06050A 19083.60036133 .00000000 00000-0 23239-4 0 9997
2 29522 98.8260 101.1948 0010475 26.0695 334.1004 14.14004541639023
| Epoch (UTC): | 24 March 2019 14:24:31 |
| Eccentricity: | 0.0010475 |
| inclination: | 98.8260° |
| perigee height: | 838 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 101.1948° |
| argument of perigee: | 26.0695° |
| revolutions per day: | 14.14004541 |
| mean anomaly at epoch: | 334.1004° |
| orbit number at epoch: | 63902 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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