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 08110U 26100.20846720 +.00000000 +00000-0 +98013-4 0 00006
2 08110 81.3501 188.2291 0032972 200.1544 159.8329 14.11478349 09
| Epoch (UTC): | 10 April 2026 05:00:11 |
| Eccentricity: | 0.0032972 |
| inclination: | 81.3501° |
| perigee height: | 830 km |
| apogee height: | 878 km |
| right ascension of ascending node: | 188.2291° |
| argument of perigee: | 200.1544° |
| revolutions per day: | 14.11478349 |
| mean anomaly at epoch: | 159.8329° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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