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 23153.85972173 .00000190 00000-0 85939-4 0 9990
2 20442 98.8429 130.0700 0010979 216.4478 143.5959 14.33257663743294
| Epoch (UTC): | 02 June 2023 20:37:59 |
| Eccentricity: | 0.0010979 |
| inclination: | 98.8429° |
| perigee height: | 773 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 130.0700° |
| argument of perigee: | 216.4478° |
| revolutions per day: | 14.33257663 |
| mean anomaly at epoch: | 143.5959° |
| orbit number at epoch: | 74329 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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