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 23086.91023204 .00000466 00000-0 18620-3 0 9992
2 20442 98.8366 61.7246 0012764 59.9139 300.3308 14.33209525733707
| Epoch (UTC): | 27 March 2023 21:50:44 |
| Eccentricity: | 0.0012764 |
| inclination: | 98.8366° |
| perigee height: | 772 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 61.7246° |
| argument of perigee: | 59.9139° |
| revolutions per day: | 14.33209525 |
| mean anomaly at epoch: | 300.3308° |
| orbit number at epoch: | 73370 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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