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 25198.43370413 .00001785 00000-0 88253-4 0 9999
2 33505 82.3849 182.2982 0023474 109.5861 250.7909 15.16957054906655
| Epoch (UTC): | 17 July 2025 10:24:32 |
| Eccentricity: | 0.0023474 |
| inclination: | 82.3849° |
| perigee height: | 499 km |
| apogee height: | 531 km |
| right ascension of ascending node: | 182.2982° |
| argument of perigee: | 109.5861° |
| revolutions per day: | 15.16957054 |
| mean anomaly at epoch: | 250.7909° |
| orbit number at epoch: | 90665 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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