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 18986U 26100.45844125 +.00000000 +00000-0 +28194-4 0 00005
2 18986 82.9568 167.9763 0041845 176.5289 183.6168 13.78937070 09
| Epoch (UTC): | 10 April 2026 11:00:09 |
| Eccentricity: | 0.0041845 |
| inclination: | 82.9568° |
| perigee height: | 937 km |
| apogee height: | 998 km |
| right ascension of ascending node: | 167.9763° |
| argument of perigee: | 176.5289° |
| revolutions per day: | 13.78937070 |
| mean anomaly at epoch: | 183.6168° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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