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 05118U 71028B 25199.90673923 .00016215 00000-0 32607-3 0 9994
2 05118 81.2430 337.0105 0023980 35.6241 324.6598 15.46166108952390
| Epoch (UTC): | 18 July 2025 21:45:42 |
| Eccentricity: | 0.0023980 |
| inclination: | 81.2430° |
| perigee height: | 411 km |
| apogee height: | 444 km |
| right ascension of ascending node: | 337.0105° |
| argument of perigee: | 35.6241° |
| revolutions per day: | 15.46166108 |
| mean anomaly at epoch: | 324.6598° |
| orbit number at epoch: | 95239 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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