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 18187U 26017.30245279 +.00000000 +00000-0 +17990-4 0 00006
2 18187 65.0109 90.6138 0013881 274.5560 85.3939 14.31492965 06
| Epoch (UTC): | 17 January 2026 07:15:31 |
| Eccentricity: | 0.0013881 |
| inclination: | 65.0109° |
| perigee height: | 777 km |
| apogee height: | 797 km |
| right ascension of ascending node: | 90.6138° |
| argument of perigee: | 274.5560° |
| revolutions per day: | 14.31492965 |
| mean anomaly at epoch: | 85.3939° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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