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 22565U 93016A 25199.70303041 -.00000306 00000-0 -13939-3 0 9992
2 22565 70.7860 298.3330 0005923 19.6178 340.5168 14.12445158666267
| Epoch (UTC): | 18 July 2025 16:52:21 |
| Eccentricity: | 0.0005923 |
| inclination: | 70.7860° |
| perigee height: | 847 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 298.3330° |
| argument of perigee: | 19.6178° |
| revolutions per day: | 14.12445158 |
| mean anomaly at epoch: | 340.5168° |
| orbit number at epoch: | 66626 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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