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 20717U 90063C 24281.46713304 .00002160 00000-0 51801-2 0 9996
2 20717 4.3719 19.9936 7158036 238.6826 32.6311 2.35746550281919
| Epoch (UTC): | 07 October 2024 11:12:40 |
| Eccentricity: | 0.7158036 |
| inclination: | 4.3719° |
| perigee height: | 399 km |
| apogee height: | 34539 km |
| right ascension of ascending node: | 19.9936° |
| argument of perigee: | 238.6826° |
| revolutions per day: | 2.35746550 |
| mean anomaly at epoch: | 32.6311° |
| orbit number at epoch: | 28191 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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