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 13242U 82051B 25194.49579409 .00000162 00000-0 63161-4 0 9996
2 13242 74.0446 341.1758 0024468 179.6506 180.4669 14.37179272256882
| Epoch (UTC): | 13 July 2025 11:53:56 |
| Eccentricity: | 0.0024468 |
| inclination: | 74.0446° |
| perigee height: | 750 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 341.1758° |
| argument of perigee: | 179.6506° |
| revolutions per day: | 14.37179272 |
| mean anomaly at epoch: | 180.4669° |
| orbit number at epoch: | 25688 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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