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 11256U 26150.07843876 +.00000000 +00000-0 +00000-0 0 00005
2 11256 9.7295 276.9042 1784742 139.3817 254.2843 1.01529406 00
| Epoch (UTC): | 30 May 2026 01:52:57 |
| Eccentricity: | 0.1784742 |
| inclination: | 9.7295° |
| perigee height: | 27975 km |
| apogee height: | 42901 km |
| right ascension of ascending node: | 276.9042° |
| argument of perigee: | 139.3817° |
| revolutions per day: | 1.01529406 |
| mean anomaly at epoch: | 254.2843° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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