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 15032U 84056B 25189.13948431 .00000131 00000-0 54046-4 0 9990
2 15032 74.0699 93.6490 0017924 234.9836 124.9635 14.35943598149068
| Epoch (UTC): | 08 July 2025 03:20:51 |
| Eccentricity: | 0.0017924 |
| inclination: | 74.0699° |
| perigee height: | 759 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 93.6490° |
| argument of perigee: | 234.9836° |
| revolutions per day: | 14.35943598 |
| mean anomaly at epoch: | 124.9635° |
| orbit number at epoch: | 14906 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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