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 42794U 17036AF 19340.85742976 +.00000330 +00000-0 +34232-4 0 9992
2 42794 097.5190 017.8341 0124958 291.2578 067.5334 14.91180986133840
| Epoch (UTC): | 06 December 2019 20:34:41 |
| Eccentricity: | 0.0124958 |
| inclination: | 97.5190° |
| perigee height: | 507 km |
| apogee height: | 681 km |
| right ascension of ascending node: | 17.8341° |
| argument of perigee: | 291.2578° |
| revolutions per day: | 14.91180986 |
| mean anomaly at epoch: | 67.5334° |
| orbit number at epoch: | 13384 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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