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 5118U 71028B 25198.74182356 .00016114 00000-0 32447-3 0 9990
2 5118 81.2433 338.4163 0024049 39.7492 320.5509 15.46125388952507
| Epoch (UTC): | 17 July 2025 17:48:13 |
| Eccentricity: | 0.0024049 |
| inclination: | 81.2433° |
| perigee height: | 412 km |
| apogee height: | 444 km |
| right ascension of ascending node: | 338.4163° |
| argument of perigee: | 39.7492° |
| revolutions per day: | 15.46125388 |
| mean anomaly at epoch: | 320.5509° |
| orbit number at epoch: | 95250 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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