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 42932U 17052A 19290.22574643 0.00000000 00000-0 00000-0 0 02
2 42932 54.5181 335.2238 0010332 254.4306 105.5693 15.84702038 02
| Epoch (UTC): | 17 October 2019 05:25:04 |
| Eccentricity: | 0.0010332 |
| inclination: | 54.5181° |
| perigee height: | 310 km |
| apogee height: | 324 km |
| right ascension of ascending node: | 335.2238° |
| argument of perigee: | 254.4306° |
| revolutions per day: | 15.84702038 |
| mean anomaly at epoch: | 105.5693° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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