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 19340.61694151 .00000119 00000-0 31706-4 0 9996
2 28895 97.9826 117.7494 0017164 168.0740 192.0872 14.63717928752486
| Epoch (UTC): | 06 December 2019 14:48:23 |
| Eccentricity: | 0.0017164 |
| inclination: | 97.9826° |
| perigee height: | 669 km |
| apogee height: | 693 km |
| right ascension of ascending node: | 117.7494° |
| argument of perigee: | 168.0740° |
| revolutions per day: | 14.63717928 |
| mean anomaly at epoch: | 192.0872° |
| orbit number at epoch: | 75248 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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