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 23090.81975927 .00000521 00000-0 20627-3 0 9996
2 20442 98.8370 65.7135 0012630 49.2522 310.9756 14.33213852734324
| Epoch (UTC): | 31 March 2023 19:40:27 |
| Eccentricity: | 0.0012630 |
| inclination: | 98.8370° |
| perigee height: | 772 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 65.7135° |
| argument of perigee: | 49.2522° |
| revolutions per day: | 14.33213852 |
| mean anomaly at epoch: | 310.9756° |
| orbit number at epoch: | 73432 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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