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 20480U 90013C 23270.82474902 .00000002 00000-0 83742-4 0 9997
2 20480 99.0738 4.4205 0539482 235.2176 119.7019 12.83448845575949
| Epoch (UTC): | 27 September 2023 19:47:38 |
| Eccentricity: | 0.0539482 |
| inclination: | 99.0738° |
| perigee height: | 912 km |
| apogee height: | 1743 km |
| right ascension of ascending node: | 4.4205° |
| argument of perigee: | 235.2176° |
| revolutions per day: | 12.83448845 |
| mean anomaly at epoch: | 119.7019° |
| orbit number at epoch: | 57594 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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