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 23336.89671773 .00000413 00000-0 16634-3 0 9992
2 20442 98.8650 317.2017 0012556 47.6644 312.5600 14.33382026769518
| Epoch (UTC): | 02 December 2023 21:31:16 |
| Eccentricity: | 0.0012556 |
| inclination: | 98.8650° |
| perigee height: | 771 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 317.2017° |
| argument of perigee: | 47.6644° |
| revolutions per day: | 14.33382026 |
| mean anomaly at epoch: | 312.5600° |
| orbit number at epoch: | 76951 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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