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 24259.95623123 .00000896 00000-0 33969-3 0 9995
2 20442 98.8906 252.6469 0010490 281.1127 78.8877 14.33661476810784
| Epoch (UTC): | 15 September 2024 22:56:58 |
| Eccentricity: | 0.0010490 |
| inclination: | 98.8906° |
| perigee height: | 772 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 252.6469° |
| argument of perigee: | 281.1127° |
| revolutions per day: | 14.33661476 |
| mean anomaly at epoch: | 78.8877° |
| orbit number at epoch: | 81078 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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