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 22175.78123161 .00000063 00000-0 39788-4 0 9990
2 20442 98.7940 140.7545 0012347 142.8205 217.3836 14.33065942694215
| Epoch (UTC): | 24 June 2022 18:44:58 |
| Eccentricity: | 0.0012347 |
| inclination: | 98.7940° |
| perigee height: | 772 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 140.7545° |
| argument of perigee: | 142.8205° |
| revolutions per day: | 14.33065942 |
| mean anomaly at epoch: | 217.3836° |
| orbit number at epoch: | 69421 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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