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 22230.19338008 .00000015 00000-0 28793-4 0 9994
2 25732 98.8501 271.3386 0038360 110.6229 291.8830 14.17740178204145
| Epoch (UTC): | 18 August 2022 04:38:28 |
| Eccentricity: | 0.0038360 |
| inclination: | 98.8501° |
| perigee height: | 805 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 271.3386° |
| argument of perigee: | 110.6229° |
| revolutions per day: | 14.17740178 |
| mean anomaly at epoch: | 291.8830° |
| orbit number at epoch: | 20414 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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