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 is defined by the following mean orbital elements,
1 17755U 26100.03767228 +.00000000 +00000-0 +51057-4 0 00004
2 17755 81.2510 92.4758 0068801 186.0418 237.0116 14.14698101 05
| Epoch (UTC): | 10 April 2026 00:54:14 |
| Eccentricity: | 0.0068801 |
| inclination: | 81.2510° |
| perigee height: | 794 km |
| apogee height: | 893 km |
| right ascension of ascending node: | 92.4758° |
| argument of perigee: | 186.0418° |
| revolutions per day: | 14.14698101 |
| mean anomaly at epoch: | 237.0116° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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