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 26070.22704906 +.00000000 +00000-0 +71783-4 0 00006
2 18153 82.5030 347.5829 0021036 12.7804 347.3941 14.85631545 03
| Epoch (UTC): | 11 March 2026 05:26:57 |
| Eccentricity: | 0.0021036 |
| inclination: | 82.5030° |
| perigee height: | 597 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 347.5829° |
| argument of perigee: | 12.7804° |
| revolutions per day: | 14.85631545 |
| mean anomaly at epoch: | 347.3941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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