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 23161.09976281 .00000099 00000-0 69597-4 0 9997
2 25732 98.8035 205.4173 0036990 346.4280 33.9394 14.17825820246078
| Epoch (UTC): | 10 June 2023 02:23:39 |
| Eccentricity: | 0.0036990 |
| inclination: | 98.8035° |
| perigee height: | 806 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 205.4173° |
| argument of perigee: | 346.4280° |
| revolutions per day: | 14.17825820 |
| mean anomaly at epoch: | 33.9394° |
| orbit number at epoch: | 24607 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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