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 5485U 71080A 19113.35602290 -.00000009 +00000-0 -44538-4 0 9999
2 5485 032.0530 243.0593 0640268 051.8595 313.7968 12.74131904215986
| Epoch (UTC): | 23 April 2019 08:32:40 |
| Eccentricity: | 0.0640268 |
| inclination: | 32.0530° |
| perigee height: | 869 km |
| apogee height: | 1861 km |
| right ascension of ascending node: | 243.0593° |
| argument of perigee: | 51.8595° |
| revolutions per day: | 12.74131904 |
| mean anomaly at epoch: | 313.7968° |
| orbit number at epoch: | 21598 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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