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 25520U 98064B 19345.21887734 +.00000582 +00000-0 +12238-4 0 9998
2 25520 028.4639 281.7110 0005031 351.4118 008.6391 15.29321703172932
| Epoch (UTC): | 11 December 2019 05:15:11 |
| Eccentricity: | 0.0005031 |
| inclination: | 28.4639° |
| perigee height: | 474 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 281.7110° |
| argument of perigee: | 351.4118° |
| revolutions per day: | 15.29321703 |
| mean anomaly at epoch: | 8.6391° |
| orbit number at epoch: | 17293 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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