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 11289U 79021B 25198.38923299 .00000062 00000-0 25938-4 0 9999
2 11289 81.2468 163.4091 0075862 134.2758 226.4673 14.12035494387106
| Epoch (UTC): | 17 July 2025 09:20:29 |
| Eccentricity: | 0.0075862 |
| inclination: | 81.2468° |
| perigee height: | 797 km |
| apogee height: | 907 km |
| right ascension of ascending node: | 163.4091° |
| argument of perigee: | 134.2758° |
| revolutions per day: | 14.12035494 |
| mean anomaly at epoch: | 226.4673° |
| orbit number at epoch: | 38710 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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