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 25107.73082603 .00000169 00000-0 10293-3 0 9992
2 25732 98.7060 153.8898 0036838 200.1785 269.0447 14.18172251341961
| Epoch (UTC): | 17 April 2025 17:32:23 |
| Eccentricity: | 0.0036838 |
| inclination: | 98.7060° |
| perigee height: | 805 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 153.8898° |
| argument of perigee: | 200.1785° |
| revolutions per day: | 14.18172251 |
| mean anomaly at epoch: | 269.0447° |
| orbit number at epoch: | 34196 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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