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 28485U 04047A 19321.65306734 +.00000791 +00000-0 +23585-4 0 9996
2 28485 020.5570 074.4329 0010989 245.6346 114.2940 15.04483561821407
| Epoch (UTC): | 17 November 2019 15:40:25 |
| Eccentricity: | 0.0010989 |
| inclination: | 20.5570° |
| perigee height: | 545 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 74.4329° |
| argument of perigee: | 245.6346° |
| revolutions per day: | 15.04483561 |
| mean anomaly at epoch: | 114.2940° |
| orbit number at epoch: | 82140 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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