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 18009U 26140.51442515 +.00000000 +00000-0 +40437-3 0 00002
2 18009 63.2938 75.1435 0784989 104.7484 264.1827 13.86744569 02
| Epoch (UTC): | 20 May 2026 12:20:46 |
| Eccentricity: | 0.0784989 |
| inclination: | 63.2938° |
| perigee height: | 366 km |
| apogee height: | 1515 km |
| right ascension of ascending node: | 75.1435° |
| argument of perigee: | 104.7484° |
| revolutions per day: | 13.86744569 |
| mean anomaly at epoch: | 264.1827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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