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 56171U 26145.35412872 +.00000000 +00000-0 +12170-3 0 00007
2 56171 81.0012 102.4670 0017015 11.1206 349.0321 13.82654866 00
| Epoch (UTC): | 25 May 2026 08:29:56 |
| Eccentricity: | 0.0017015 |
| inclination: | 81.0012° |
| perigee height: | 942 km |
| apogee height: | 967 km |
| right ascension of ascending node: | 102.4670° |
| argument of perigee: | 11.1206° |
| revolutions per day: | 13.82654866 |
| mean anomaly at epoch: | 349.0321° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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