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 20439U 90005D 23083.20202727 .00001151 00000-0 43652-3 0 9991
2 20439 98.8791 71.2760 0011913 92.2586 331.7685 14.33056419732980
| Epoch (UTC): | 24 March 2023 04:50:55 |
| Eccentricity: | 0.0011913 |
| inclination: | 98.8791° |
| perigee height: | 773 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 71.2760° |
| argument of perigee: | 92.2586° |
| revolutions per day: | 14.33056419 |
| mean anomaly at epoch: | 331.7685° |
| orbit number at epoch: | 73298 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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