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 09482U 76102B 25196.93243310 .00000206 00000-0 10944-3 0 9996
2 09482 81.2557 135.6328 0085950 114.2465 246.7715 14.07912487502700
| Epoch (UTC): | 15 July 2025 22:22:42 |
| Eccentricity: | 0.0085950 |
| inclination: | 81.2557° |
| perigee height: | 804 km |
| apogee height: | 929 km |
| right ascension of ascending node: | 135.6328° |
| argument of perigee: | 114.2465° |
| revolutions per day: | 14.07912487 |
| mean anomaly at epoch: | 246.7715° |
| orbit number at epoch: | 50270 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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