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 22179.90062512 .00000027 00000-0 26660-4 0 9995
2 20442 98.7943 144.9370 0012559 131.4438 228.7826 14.33066773694743
| Epoch (UTC): | 28 June 2022 21:36:54 |
| Eccentricity: | 0.0012559 |
| inclination: | 98.7943° |
| perigee height: | 772 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 144.9370° |
| argument of perigee: | 131.4438° |
| revolutions per day: | 14.33066773 |
| mean anomaly at epoch: | 228.7826° |
| orbit number at epoch: | 69474 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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