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 42844U 17042V 19341.50196831 .00000443 00000-0 48723-4 0 9996
2 42844 97.5440 228.2570 0011961 189.4387 170.6610 14.92182567130625
| Epoch (UTC): | 07 December 2019 12:02:50 |
| Eccentricity: | 0.0011961 |
| inclination: | 97.5440° |
| perigee height: | 583 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 228.2570° |
| argument of perigee: | 189.4387° |
| revolutions per day: | 14.92182567 |
| mean anomaly at epoch: | 170.6610° |
| orbit number at epoch: | 13062 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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