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 25189.20915307 .00000130 00000-0 53859-4 0 9994
2 15032 74.0699 93.5214 0017923 234.8524 125.0950 14.35943620148813
| Epoch (UTC): | 08 July 2025 05:01:10 |
| Eccentricity: | 0.0017923 |
| inclination: | 74.0699° |
| perigee height: | 759 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 93.5214° |
| argument of perigee: | 234.8524° |
| revolutions per day: | 14.35943620 |
| mean anomaly at epoch: | 125.0950° |
| orbit number at epoch: | 14881 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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