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 56052U 26145.51986060 +.00000000 +00000-0 +55181-4 0 00008
2 56052 87.9252 248.4882 0002088 94.6728 265.4645 13.21824808 02
| Epoch (UTC): | 25 May 2026 12:28:35 |
| Eccentricity: | 0.0002088 |
| inclination: | 87.9252° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4882° |
| argument of perigee: | 94.6728° |
| revolutions per day: | 13.21824808 |
| mean anomaly at epoch: | 265.4645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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