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 25400U 98043G 25193.55591943 .00000025 00000-0 29556-4 0 9994
2 25400 98.7885 140.7404 0009799 357.8578 2.2558 14.25977325404763
| Epoch (UTC): | 12 July 2025 13:20:31 |
| Eccentricity: | 0.0009799 |
| inclination: | 98.7885° |
| perigee height: | 798 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 140.7404° |
| argument of perigee: | 357.8578° |
| revolutions per day: | 14.25977325 |
| mean anomaly at epoch: | 2.2558° |
| orbit number at epoch: | 40476 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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