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 28895U 05043F 18175.38657438 +.00000122 +00000-0 +32279-4 0 9992
2 28895 097.9098 326.5506 0017866 050.2687 310.0087 14.63556168674932
| Epoch (UTC): | 24 June 2018 09:16:40 |
| Eccentricity: | 0.0017866 |
| inclination: | 97.9098° |
| perigee height: | 669 km |
| apogee height: | 694 km |
| right ascension of ascending node: | 326.5506° |
| argument of perigee: | 50.2687° |
| revolutions per day: | 14.63556168 |
| mean anomaly at epoch: | 310.0087° |
| orbit number at epoch: | 67493 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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