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 20580U 90037B 24277.88046536 .00019870 00000-0 88934-3 0 9996
2 20580 28.4698 335.8650 0003247 142.9508 217.1310 15.19890521693575
| Epoch (UTC): | 03 October 2024 21:07:52 |
| Eccentricity: | 0.0003247 |
| inclination: | 28.4698° |
| perigee height: | 504 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 335.8650° |
| argument of perigee: | 142.9508° |
| revolutions per day: | 15.19890521 |
| mean anomaly at epoch: | 217.1310° |
| orbit number at epoch: | 69357 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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