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 20253U 89077A 23080.77272701 -.00000090 00000-0 00000-0 0 9999
2 20253 12.7773 358.4030 0003561 91.2467 79.3946 1.00272525248745
| Epoch (UTC): | 21 March 2023 18:32:43 |
| Eccentricity: | 0.0003561 |
| inclination: | 12.7773° |
| perigee height: | 35771 km |
| apogee height: | 35801 km |
| right ascension of ascending node: | 358.4030° |
| argument of perigee: | 91.2467° |
| revolutions per day: | 1.00272525 |
| mean anomaly at epoch: | 79.3946° |
| orbit number at epoch: | 24874 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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