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 56065U 26145.49049155 +.00000000 +00000-0 +72621-3 0 00001
2 56065 87.9106 233.2809 0002315 98.9861 261.1532 13.16599793 07
| Epoch (UTC): | 25 May 2026 11:46:18 |
| Eccentricity: | 0.0002315 |
| inclination: | 87.9106° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2809° |
| argument of perigee: | 98.9861° |
| revolutions per day: | 13.16599793 |
| mean anomaly at epoch: | 261.1532° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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