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 26105.39259138 +.00000000 +00000-0 +27432-4 0 00001
2 18986 82.9559 164.3046 0042172 162.8008 197.4591 13.78937185 05
| Epoch (UTC): | 15 April 2026 09:25:19 |
| Eccentricity: | 0.0042172 |
| inclination: | 82.9559° |
| perigee height: | 937 km |
| apogee height: | 999 km |
| right ascension of ascending node: | 164.3046° |
| argument of perigee: | 162.8008° |
| revolutions per day: | 13.78937185 |
| mean anomaly at epoch: | 197.4591° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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