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 2389U 66070A 19112.52561016 .00001837 00000-0 98475-4 0 9997
2 2389 81.3882 343.7764 1239044 101.6617 272.5900 12.92979598256877
| Epoch (UTC): | 22 April 2019 12:36:52 |
| Eccentricity: | 0.1239044 |
| inclination: | 81.3882° |
| perigee height: | 339 km |
| apogee height: | 2240 km |
| right ascension of ascending node: | 343.7764° |
| argument of perigee: | 101.6617° |
| revolutions per day: | 12.92979598 |
| mean anomaly at epoch: | 272.5900° |
| orbit number at epoch: | 25687 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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