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 23153.56973737 .00000096 00000-0 68491-4 0 9992
2 25732 98.8041 197.9511 0037407 8.0343 119.3630 14.17823795244867
| Epoch (UTC): | 02 June 2023 13:40:25 |
| Eccentricity: | 0.0037407 |
| inclination: | 98.8041° |
| perigee height: | 806 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 197.9511° |
| argument of perigee: | 8.0343° |
| revolutions per day: | 14.17823795 |
| mean anomaly at epoch: | 119.3630° |
| orbit number at epoch: | 24486 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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