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 39417U 13066B 24276.62398637 .00018964 00000-0 18594-2 0 9992
2 39417 97.7454 230.3785 0049365 161.8374 198.4622 14.91350216587584
| Epoch (UTC): | 02 October 2024 14:58:32 |
| Eccentricity: | 0.0049365 |
| inclination: | 97.7454° |
| perigee height: | 559 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 230.3785° |
| argument of perigee: | 161.8374° |
| revolutions per day: | 14.91350216 |
| mean anomaly at epoch: | 198.4622° |
| orbit number at epoch: | 58758 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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