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 26162.60461154 +.00000000 +00000-0 -58855-4 0 00005
2 10515 81.2436 330.8579 0022262 348.7182 11.3486 14.09111652 03
| Epoch (UTC): | 11 June 2026 14:30:38 |
| Eccentricity: | 0.0022262 |
| inclination: | 81.2436° |
| perigee height: | 846 km |
| apogee height: | 879 km |
| right ascension of ascending node: | 330.8579° |
| argument of perigee: | 348.7182° |
| revolutions per day: | 14.09111652 |
| mean anomaly at epoch: | 11.3486° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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