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 25196.89726428 .00003294 00000-0 14385-3 0 9998
2 13403 81.1481 111.9827 0024815 244.7618 115.1041 15.21565888341658
| Epoch (UTC): | 15 July 2025 21:32:03 |
| Eccentricity: | 0.0024815 |
| inclination: | 81.1481° |
| perigee height: | 484 km |
| apogee height: | 518 km |
| right ascension of ascending node: | 111.9827° |
| argument of perigee: | 244.7618° |
| revolutions per day: | 15.21565888 |
| mean anomaly at epoch: | 115.1041° |
| orbit number at epoch: | 34165 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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