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 42728U 98067MH 19047.60446742 .14892182 12584-4 44484-3 0 9993
2 42728 51.6170 162.9558 0004113 309.3568 50.8266 16.45061398 99080
| Epoch (UTC): | 16 February 2019 14:30:25 |
| Eccentricity: | 0.0004113 |
| inclination: | 51.6170° |
| perigee height: | 149 km |
| apogee height: | 155 km |
| right ascension of ascending node: | 162.9558° |
| argument of perigee: | 309.3568° |
| revolutions per day: | 16.45061398 |
| mean anomaly at epoch: | 50.8266° |
| orbit number at epoch: | 9908 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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