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 26032.13633704 +.00000000 +00000-0 +15864-3 0 00009
2 18361 90.3683 81.1443 0105780 80.6195 280.6893 13.44917848 06
| Epoch (UTC): | 01 February 2026 03:16:19 |
| Eccentricity: | 0.0105780 |
| inclination: | 90.3683° |
| perigee height: | 1012 km |
| apogee height: | 1170 km |
| right ascension of ascending node: | 81.1443° |
| argument of perigee: | 80.6195° |
| revolutions per day: | 13.44917848 |
| mean anomaly at epoch: | 280.6893° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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