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 41932U 98067KU 19003.69298287 .08988731 12526-4 32153-3 0 9994
2 41932 51.6105 8.9412 0001311 269.7383 90.3495 16.44586236112635
| Epoch (UTC): | 03 January 2019 16:37:53 |
| Eccentricity: | 0.0001311 |
| inclination: | 51.6105° |
| perigee height: | 153 km |
| apogee height: | 154 km |
| right ascension of ascending node: | 8.9412° |
| argument of perigee: | 269.7383° |
| revolutions per day: | 16.44586236 |
| mean anomaly at epoch: | 90.3495° |
| orbit number at epoch: | 11263 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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