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 24280.44124272 .00016639 00000-0 74174-3 0 9997
2 20580 28.4698 318.6513 0003112 169.3583 190.7076 15.19975280693963
| Epoch (UTC): | 06 October 2024 10:35:23 |
| Eccentricity: | 0.0003112 |
| inclination: | 28.4698° |
| perigee height: | 504 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 318.6513° |
| argument of perigee: | 169.3583° |
| revolutions per day: | 15.19975280 |
| mean anomaly at epoch: | 190.7076° |
| orbit number at epoch: | 69396 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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