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 38819U 99025EVK 22175.81118954 .00000411 00000-0 22462-3 0 9993
2 38819 98.6067 193.2579 0083131 239.6174 296.4788 14.15563257455323
| Epoch (UTC): | 24 June 2022 19:28:06 |
| Eccentricity: | 0.0083131 |
| inclination: | 98.6067° |
| perigee height: | 780 km |
| apogee height: | 900 km |
| right ascension of ascending node: | 193.2579° |
| argument of perigee: | 239.6174° |
| revolutions per day: | 14.15563257 |
| mean anomaly at epoch: | 296.4788° |
| orbit number at epoch: | 45532 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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