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 43758U 26111.87424024 +.00000000 +00000-0 +68046-3 0 00009
2 43758 97.4557 186.6660 0009233 112.7660 247.4564 15.43238093 09
| Epoch (UTC): | 21 April 2026 20:58:54 |
| Eccentricity: | 0.0009233 |
| inclination: | 97.4557° |
| perigee height: | 430 km |
| apogee height: | 443 km |
| right ascension of ascending node: | 186.6660° |
| argument of perigee: | 112.7660° |
| revolutions per day: | 15.43238093 |
| mean anomaly at epoch: | 247.4564° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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