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 26159.47384328 +.00000000 +00000-0 +17219-3 0 00002
2 10517 28.6583 80.9806 0812828 157.0663 206.8399 13.47689062 09
| Epoch (UTC): | 08 June 2026 11:22:20 |
| Eccentricity: | 0.0812828 |
| inclination: | 28.6583° |
| perigee height: | 474 km |
| apogee height: | 1687 km |
| right ascension of ascending node: | 80.9806° |
| argument of perigee: | 157.0663° |
| revolutions per day: | 13.47689062 |
| mean anomaly at epoch: | 206.8399° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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