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 25196.91654427 .00001526 00000-0 75203-4 0 9994
2 33505 82.3847 183.8220 0023420 114.5203 245.8475 15.16951400906429
| Epoch (UTC): | 15 July 2025 21:59:49 |
| Eccentricity: | 0.0023420 |
| inclination: | 82.3847° |
| perigee height: | 499 km |
| apogee height: | 531 km |
| right ascension of ascending node: | 183.8220° |
| argument of perigee: | 114.5203° |
| revolutions per day: | 15.16951400 |
| mean anomaly at epoch: | 245.8475° |
| orbit number at epoch: | 90642 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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