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 18361U 26142.24456100 +.00000000 +00000-0 +15731-3 0 00009
2 18361 90.3712 85.1866 0105424 124.0723 237.0486 13.44936790 08
| Epoch (UTC): | 22 May 2026 05:52:10 |
| Eccentricity: | 0.0105424 |
| inclination: | 90.3712° |
| perigee height: | 1012 km |
| apogee height: | 1170 km |
| right ascension of ascending node: | 85.1866° |
| argument of perigee: | 124.0723° |
| revolutions per day: | 13.44936790 |
| mean anomaly at epoch: | 237.0486° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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