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 20692U 90050D 24277.15680163 .00013655 00000-0 10907-2 0 9994
2 20692 63.2981 80.3798 0904257 72.8812 296.9145 13.54433636 20118
| Epoch (UTC): | 03 October 2024 03:45:47 |
| Eccentricity: | 0.0904257 |
| inclination: | 63.2981° |
| perigee height: | 384 km |
| apogee height: | 1728 km |
| right ascension of ascending node: | 80.3798° |
| argument of perigee: | 72.8812° |
| revolutions per day: | 13.54433636 |
| mean anomaly at epoch: | 296.9145° |
| orbit number at epoch: | 2011 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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