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 40340U 26145.61471605 +.00000000 +00000-0 +17284-3 0 00007
2 40340 63.3889 9.4467 0364895 9.5301 351.2407 13.45347682 08
| Epoch (UTC): | 25 May 2026 14:45:11 |
| Eccentricity: | 0.0364895 |
| inclination: | 63.3889° |
| perigee height: | 817 km |
| apogee height: | 1362 km |
| right ascension of ascending node: | 9.4467° |
| argument of perigee: | 9.5301° |
| revolutions per day: | 13.45347682 |
| mean anomaly at epoch: | 351.2407° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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