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 26073.45998417 +.00000000 +00000-0 +61428-4 0 00001
2 18153 82.5029 344.5368 0020722 2.3194 357.8114 14.85635434 03
| Epoch (UTC): | 14 March 2026 11:02:22 |
| Eccentricity: | 0.0020722 |
| inclination: | 82.5029° |
| perigee height: | 597 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 344.5368° |
| argument of perigee: | 2.3194° |
| revolutions per day: | 14.85635434 |
| mean anomaly at epoch: | 357.8114° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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