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 26037.63322800 +.00000000 +00000-0 -20095-4 0 00008
2 10515 81.2418 92.3189 0026733 344.3689 15.6653 14.09095428 06
| Epoch (UTC): | 06 February 2026 15:11:50 |
| Eccentricity: | 0.0026733 |
| inclination: | 81.2418° |
| perigee height: | 843 km |
| apogee height: | 882 km |
| right ascension of ascending node: | 92.3189° |
| argument of perigee: | 344.3689° |
| revolutions per day: | 14.09095428 |
| mean anomaly at epoch: | 15.6653° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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