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 24282.73924771 .00026727 00000-0 11920-2 0 9991
2 20580 28.4694 303.2008 0002947 192.3580 167.6942 15.20070792694317
| Epoch (UTC): | 08 October 2024 17:44:31 |
| Eccentricity: | 0.0002947 |
| inclination: | 28.4694° |
| perigee height: | 503 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 303.2008° |
| argument of perigee: | 192.3580° |
| revolutions per day: | 15.20070792 |
| mean anomaly at epoch: | 167.6942° |
| orbit number at epoch: | 69431 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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