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 20509U 90017B 24357.77787299 .00000105 00000-0 91633-4 0 9992
2 20509 82.9536 92.1038 0043918 54.7635 305.7620 13.75796199747793
| Epoch (UTC): | 22 December 2024 18:40:08 |
| Eccentricity: | 0.0043918 |
| inclination: | 82.9536° |
| perigee height: | 946 km |
| apogee height: | 1011 km |
| right ascension of ascending node: | 92.1038° |
| argument of perigee: | 54.7635° |
| revolutions per day: | 13.75796199 |
| mean anomaly at epoch: | 305.7620° |
| orbit number at epoch: | 74779 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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