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 23085.93284830 .00000493 00000-0 19614-3 0 9991
2 20442 98.8364 60.7275 0012782 62.5459 297.7022 14.33208654733569
| Epoch (UTC): | 26 March 2023 22:23:18 |
| Eccentricity: | 0.0012782 |
| inclination: | 98.8364° |
| perigee height: | 772 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 60.7275° |
| argument of perigee: | 62.5459° |
| revolutions per day: | 14.33208654 |
| mean anomaly at epoch: | 297.7022° |
| orbit number at epoch: | 73356 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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