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 23089.77256564 .00000531 00000-0 20965-3 0 9994
2 20442 98.8369 64.6451 0012666 52.1047 308.1280 14.33212847734116
| Epoch (UTC): | 30 March 2023 18:32:29 |
| Eccentricity: | 0.0012666 |
| inclination: | 98.8369° |
| perigee height: | 772 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 64.6451° |
| argument of perigee: | 52.1047° |
| revolutions per day: | 14.33212847 |
| mean anomaly at epoch: | 308.1280° |
| orbit number at epoch: | 73411 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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