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 56717U 26145.51901889 +.00000000 +00000-0 +11132-4 0 00000
2 56717 87.9255 248.4819 0002736 85.2043 274.9403 13.21825296 08
| Epoch (UTC): | 25 May 2026 12:27:23 |
| Eccentricity: | 0.0002736 |
| inclination: | 87.9255° |
| perigee height: | 1176 km |
| apogee height: | 1180 km |
| right ascension of ascending node: | 248.4819° |
| argument of perigee: | 85.2043° |
| revolutions per day: | 13.21825296 |
| mean anomaly at epoch: | 274.9403° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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