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 15772U 85042D 25131.83106492 .00000135 00000-0 82366-4 0 9994
2 15772 71.1096 5.4049 0037022 237.2104 196.0134 14.21878631 71488
| Epoch (UTC): | 11 May 2025 19:56:44 |
| Eccentricity: | 0.0037022 |
| inclination: | 71.1096° |
| perigee height: | 792 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 5.4049° |
| argument of perigee: | 237.2104° |
| revolutions per day: | 14.21878631 |
| mean anomaly at epoch: | 196.0134° |
| orbit number at epoch: | 7148 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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