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 33505U 09003B 25193.94817190 .00001094 00000-0 53458-4 0 9990
2 33505 82.3846 186.8032 0023312 124.2102 236.1345 15.16943219905975
| Epoch (UTC): | 12 July 2025 22:45:22 |
| Eccentricity: | 0.0023312 |
| inclination: | 82.3846° |
| perigee height: | 499 km |
| apogee height: | 531 km |
| right ascension of ascending node: | 186.8032° |
| argument of perigee: | 124.2102° |
| revolutions per day: | 15.16943219 |
| mean anomaly at epoch: | 236.1345° |
| orbit number at epoch: | 90597 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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