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 29110U 06016D 25198.74117940 .00012363 00000-0 79903-3 0 9990
2 29110 98.3487 86.2653 0006738 43.0672 42.1263 15.08366936 33012
| Epoch (UTC): | 17 July 2025 17:47:17 |
| Eccentricity: | 0.0006738 |
| inclination: | 98.3487° |
| perigee height: | 536 km |
| apogee height: | 546 km |
| right ascension of ascending node: | 86.2653° |
| argument of perigee: | 43.0672° |
| revolutions per day: | 15.08366936 |
| mean anomaly at epoch: | 42.1263° |
| orbit number at epoch: | 3301 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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