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 20440U 90005E 23341.54482799 .00000261 00000-0 11064-3 0 9999
2 20440 98.8795 330.5412 0011495 36.3130 76.6839 14.33689183770090
| Epoch (UTC): | 07 December 2023 13:04:33 |
| Eccentricity: | 0.0011495 |
| inclination: | 98.8795° |
| perigee height: | 771 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 330.5412° |
| argument of perigee: | 36.3130° |
| revolutions per day: | 14.33689183 |
| mean anomaly at epoch: | 76.6839° |
| orbit number at epoch: | 77009 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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