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 17369U 26129.35003191 +.00000000 +00000-0 +17581-4 0 00007
2 17369 65.0124 356.1849 0016370 286.2029 73.7254 14.31868540 06
| Epoch (UTC): | 09 May 2026 08:24:02 |
| Eccentricity: | 0.0016370 |
| inclination: | 65.0124° |
| perigee height: | 774 km |
| apogee height: | 797 km |
| right ascension of ascending node: | 356.1849° |
| argument of perigee: | 286.2029° |
| revolutions per day: | 14.31868540 |
| mean anomaly at epoch: | 73.7254° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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