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 18153U 26065.31027558 +.00000000 +00000-0 +89413-4 0 00000
2 18153 82.5030 352.2153 0021434 28.6582 331.5807 14.85624829 00
| Epoch (UTC): | 06 March 2026 07:26:47 |
| Eccentricity: | 0.0021434 |
| inclination: | 82.5030° |
| perigee height: | 597 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 352.2153° |
| argument of perigee: | 28.6582° |
| revolutions per day: | 14.85624829 |
| mean anomaly at epoch: | 331.5807° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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