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 42809U 17039G 23335.52966151 .00000031 00000-0 39185-5 0 9999
2 42809 86.3990 21.7368 0002053 105.7360 254.4062 14.34216883336846
| Epoch (UTC): | 01 December 2023 12:42:42 |
| Eccentricity: | 0.0002053 |
| inclination: | 86.3990° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 21.7368° |
| argument of perigee: | 105.7360° |
| revolutions per day: | 14.34216883 |
| mean anomaly at epoch: | 254.4062° |
| orbit number at epoch: | 33684 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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