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 10515U 26132.56907740 +.00000000 +00000-0 -12364-4 0 00008
2 10515 81.2464 0.0516 0024281 74.1472 286.2373 14.09114759 05
| Epoch (UTC): | 12 May 2026 13:39:28 |
| Eccentricity: | 0.0024281 |
| inclination: | 81.2464° |
| perigee height: | 845 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 0.0516° |
| argument of perigee: | 74.1472° |
| revolutions per day: | 14.09114759 |
| mean anomaly at epoch: | 286.2373° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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