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 39430U 13066Q 24357.88290835 .00004825 00000-0 77106-3 0 9992
2 39430 97.7033 220.7956 0136131 12.3650 348.0840 14.66221860590493
| Epoch (UTC): | 22 December 2024 21:11:23 |
| Eccentricity: | 0.0136131 |
| inclination: | 97.7033° |
| perigee height: | 577 km |
| apogee height: | 769 km |
| right ascension of ascending node: | 220.7956° |
| argument of perigee: | 12.3650° |
| revolutions per day: | 14.66221860 |
| mean anomaly at epoch: | 348.0840° |
| orbit number at epoch: | 59049 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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