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 26384U 26105.93044628 +.00000000 +00000-0 +70958-4 0 00009
2 26384 97.8378 83.4754 0012816 186.3371 173.7676 14.71264030 00
| Epoch (UTC): | 15 April 2026 22:19:50 |
| Eccentricity: | 0.0012816 |
| inclination: | 97.8378° |
| perigee height: | 648 km |
| apogee height: | 666 km |
| right ascension of ascending node: | 83.4754° |
| argument of perigee: | 186.3371° |
| revolutions per day: | 14.71264030 |
| mean anomaly at epoch: | 173.7676° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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