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 19077.41446097 .00000221 00000-0 27123-4 0 9999
2 42844 97.5746 334.8596 0012580 4.2694 355.8630 14.92015687 91240
| Epoch (UTC): | 18 March 2019 09:56:49 |
| Eccentricity: | 0.0012580 |
| inclination: | 97.5746° |
| perigee height: | 583 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 334.8596° |
| argument of perigee: | 4.2694° |
| revolutions per day: | 14.92015687 |
| mean anomaly at epoch: | 355.8630° |
| orbit number at epoch: | 9124 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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