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 02498U 66052C 25200.44823644 -.00000094 00000-0 -29112-4 0 9990
2 02498 40.6332 329.5153 2069196 60.8853 318.3144 10.56215003441684
| Epoch (UTC): | 19 July 2025 10:45:27 |
| Eccentricity: | 0.2069196 |
| inclination: | 40.6332° |
| perigee height: | 581 km |
| apogee height: | 4212 km |
| right ascension of ascending node: | 329.5153° |
| argument of perigee: | 60.8853° |
| revolutions per day: | 10.56215003 |
| mean anomaly at epoch: | 318.3144° |
| orbit number at epoch: | 44168 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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