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 25197.92737048 .00000213 00000-0 11388-3 0 9993
2 09482 81.2559 134.6692 0085981 111.4654 249.5712 14.07912869502845
| Epoch (UTC): | 16 July 2025 22:15:24 |
| Eccentricity: | 0.0085981 |
| inclination: | 81.2559° |
| perigee height: | 804 km |
| apogee height: | 929 km |
| right ascension of ascending node: | 134.6692° |
| argument of perigee: | 111.4654° |
| revolutions per day: | 14.07912869 |
| mean anomaly at epoch: | 249.5712° |
| orbit number at epoch: | 50284 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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