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 19197.17945338 .00000645 00000-0 13536-4 0 9996
2 28485 20.5555 225.5715 0011466 110.7909 249.3754 15.04404398802634
| Epoch (UTC): | 16 July 2019 04:18:24 |
| Eccentricity: | 0.0011466 |
| inclination: | 20.5555° |
| perigee height: | 545 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 225.5715° |
| argument of perigee: | 110.7909° |
| revolutions per day: | 15.04404398 |
| mean anomaly at epoch: | 249.3754° |
| orbit number at epoch: | 80263 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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