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 25732U 99025C 23154.56557998 .00000093 00000-0 66886-4 0 9993
2 25732 98.8041 198.9386 0037357 5.2040 162.2883 14.17823977245001
| Epoch (UTC): | 03 June 2023 13:34:26 |
| Eccentricity: | 0.0037357 |
| inclination: | 98.8041° |
| perigee height: | 806 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 198.9386° |
| argument of perigee: | 5.2040° |
| revolutions per day: | 14.17823977 |
| mean anomaly at epoch: | 162.2883° |
| orbit number at epoch: | 24500 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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