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 10517U 26044.19568861 +.00000000 +00000-0 +18571-3 0 00002
2 10517 28.6647 312.6605 0814770 276.6957 74.1614 13.47285950 08
| Epoch (UTC): | 13 February 2026 04:41:47 |
| Eccentricity: | 0.0814770 |
| inclination: | 28.6647° |
| perigee height: | 474 km |
| apogee height: | 1690 km |
| right ascension of ascending node: | 312.6605° |
| argument of perigee: | 276.6957° |
| revolutions per day: | 13.47285950 |
| mean anomaly at epoch: | 74.1614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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