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 24357.80015528 .00008737 00000-0 36431-3 0 9999
2 20580 28.4662 157.7295 0001851 316.8822 43.1627 15.21893017705750
| Epoch (UTC): | 22 December 2024 19:12:13 |
| Eccentricity: | 0.0001851 |
| inclination: | 28.4662° |
| perigee height: | 499 km |
| apogee height: | 501 km |
| right ascension of ascending node: | 157.7295° |
| argument of perigee: | 316.8822° |
| revolutions per day: | 15.21893017 |
| mean anomaly at epoch: | 43.1627° |
| orbit number at epoch: | 70575 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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