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 24258.10484428 .00020892 00000-0 16737-2 0 9992
2 20692 63.2991 131.0661 0905611 72.5072 297.2787 13.53937841 17536
| Epoch (UTC): | 14 September 2024 02:30:58 |
| Eccentricity: | 0.0905611 |
| inclination: | 63.2991° |
| perigee height: | 384 km |
| apogee height: | 1731 km |
| right ascension of ascending node: | 131.0661° |
| argument of perigee: | 72.5072° |
| revolutions per day: | 13.53937841 |
| mean anomaly at epoch: | 297.2787° |
| orbit number at epoch: | 1753 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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