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 27424U 02022A 19079.95362628 +.00000056 +00000-0 +22474-4 0 9996
2 27424 098.2105 022.1635 0001545 354.8215 070.1306 14.57101954897680
| Epoch (UTC): | 20 March 2019 22:53:13 |
| Eccentricity: | 0.0001545 |
| inclination: | 98.2105° |
| perigee height: | 701 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 22.1635° |
| argument of perigee: | 354.8215° |
| revolutions per day: | 14.57101954 |
| mean anomaly at epoch: | 70.1306° |
| orbit number at epoch: | 89768 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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