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 25509U 98061B 19082.88920031 +.00000117 +00000-0 +85459-5 0 9991
2 25509 031.4352 007.9640 0346982 259.6593 096.4746 14.30365996066990
| Epoch (UTC): | 23 March 2019 21:20:26 |
| Eccentricity: | 0.0346982 |
| inclination: | 31.4352° |
| perigee height: | 542 km |
| apogee height: | 1039 km |
| right ascension of ascending node: | 7.9640° |
| argument of perigee: | 259.6593° |
| revolutions per day: | 14.30365996 |
| mean anomaly at epoch: | 96.4746° |
| orbit number at epoch: | 6699 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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