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 25196.86495359 .00013186 00000-0 26594-3 0 9993
2 05118 81.2436 340.6807 0024194 46.2253 314.0988 15.46068792951928
| Epoch (UTC): | 15 July 2025 20:45:31 |
| Eccentricity: | 0.0024194 |
| inclination: | 81.2436° |
| perigee height: | 412 km |
| apogee height: | 445 km |
| right ascension of ascending node: | 340.6807° |
| argument of perigee: | 46.2253° |
| revolutions per day: | 15.46068792 |
| mean anomaly at epoch: | 314.0988° |
| orbit number at epoch: | 95192 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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