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 11511U 26109.37087152 +.00000000 +00000-0 +61689-4 0 00007
2 11511 74.0340 137.6332 0016420 309.5432 50.4270 14.38295993 04
| Epoch (UTC): | 19 April 2026 08:54:03 |
| Eccentricity: | 0.0016420 |
| inclination: | 74.0340° |
| perigee height: | 752 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 137.6332° |
| argument of perigee: | 309.5432° |
| revolutions per day: | 14.38295993 |
| mean anomaly at epoch: | 50.4270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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