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 25199.95085757 .00001834 00000-0 90687-4 0 9990
2 33505 82.3851 180.7745 0023553 104.7029 255.6817 15.16962565906889
| Epoch (UTC): | 18 July 2025 22:49:14 |
| Eccentricity: | 0.0023553 |
| inclination: | 82.3851° |
| perigee height: | 499 km |
| apogee height: | 531 km |
| right ascension of ascending node: | 180.7745° |
| argument of perigee: | 104.7029° |
| revolutions per day: | 15.16962565 |
| mean anomaly at epoch: | 255.6817° |
| orbit number at epoch: | 90688 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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