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 10953U 26088.13054683 +.00000000 +00000-0 +00000-0 0 00005
2 10953 7.0836 299.8902 0002382 2.9598 8.0704 0.99356954 00
| Epoch (UTC): | 29 March 2026 03:07:59 |
| Eccentricity: | 0.0002382 |
| inclination: | 7.0836° |
| perigee height: | 36035 km |
| apogee height: | 36055 km |
| right ascension of ascending node: | 299.8902° |
| argument of perigee: | 2.9598° |
| revolutions per day: | 0.99356954 |
| mean anomaly at epoch: | 8.0704° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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