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 25191.44496971 .00000020 00000-0 35085-5 0 9990
2 11289 81.2461 170.1877 0075475 153.7879 206.7145 14.12035062386123
| Epoch (UTC): | 10 July 2025 10:40:45 |
| Eccentricity: | 0.0075475 |
| inclination: | 81.2461° |
| perigee height: | 798 km |
| apogee height: | 907 km |
| right ascension of ascending node: | 170.1877° |
| argument of perigee: | 153.7879° |
| revolutions per day: | 14.12035062 |
| mean anomaly at epoch: | 206.7145° |
| orbit number at epoch: | 38612 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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