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 06393U 73015B 22144.72667091 .00000134 00000-0 74536-4 0 9995
2 06393 81.2573 10.7884 0057881 251.1662 108.3224 14.05063866519845
| Epoch (UTC): | 24 May 2022 17:26:24 |
| Eccentricity: | 0.0057881 |
| inclination: | 81.2573° |
| perigee height: | 834 km |
| apogee height: | 918 km |
| right ascension of ascending node: | 10.7884° |
| argument of perigee: | 251.1662° |
| revolutions per day: | 14.05063866 |
| mean anomaly at epoch: | 108.3224° |
| orbit number at epoch: | 51984 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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