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 13403U 82079B 25117.57140107 .00009961 00000-0 44575-3 0 9991
2 13403 81.1506 205.1258 0027591 151.7788 208.4946 15.20820015329593
| Epoch (UTC): | 27 April 2025 13:42:49 |
| Eccentricity: | 0.0027591 |
| inclination: | 81.1506° |
| perigee height: | 484 km |
| apogee height: | 522 km |
| right ascension of ascending node: | 205.1258° |
| argument of perigee: | 151.7788° |
| revolutions per day: | 15.20820015 |
| mean anomaly at epoch: | 208.4946° |
| orbit number at epoch: | 32959 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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