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 20442U 90005G 23340.52655449 .00000266 00000-0 11309-3 0 9999
2 20442 98.8653 320.9174 0012474 37.7331 322.4725 14.33384843770034
| Epoch (UTC): | 06 December 2023 12:38:14 |
| Eccentricity: | 0.0012474 |
| inclination: | 98.8653° |
| perigee height: | 771 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 320.9174° |
| argument of perigee: | 37.7331° |
| revolutions per day: | 14.33384843 |
| mean anomaly at epoch: | 322.4725° |
| orbit number at epoch: | 77003 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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