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 23334.52335816 .00000570 00000-0 22347-3 0 9997
2 20442 98.8646 314.7722 0012622 54.1150 306.1203 14.33380217769234
| Epoch (UTC): | 30 November 2023 12:33:38 |
| Eccentricity: | 0.0012622 |
| inclination: | 98.8646° |
| perigee height: | 771 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 314.7722° |
| argument of perigee: | 54.1150° |
| revolutions per day: | 14.33380217 |
| mean anomaly at epoch: | 306.1203° |
| orbit number at epoch: | 76923 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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