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 17911U 87038A 25199.87058148 .00011869 00000-0 28777-3 0 9991
2 17911 82.5106 160.5420 0008830 72.4807 287.7403 15.40874726 89190
| Epoch (UTC): | 18 July 2025 20:53:38 |
| Eccentricity: | 0.0008830 |
| inclination: | 82.5106° |
| perigee height: | 437 km |
| apogee height: | 449 km |
| right ascension of ascending node: | 160.5420° |
| argument of perigee: | 72.4807° |
| revolutions per day: | 15.40874726 |
| mean anomaly at epoch: | 287.7403° |
| orbit number at epoch: | 8919 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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