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 56799U 26145.42382994 +.00000000 +00000-0 +51286-4 0 00004
2 56799 69.9984 151.0029 0003705 267.4567 92.6168 14.98330638 00
| Epoch (UTC): | 25 May 2026 10:10:18 |
| Eccentricity: | 0.0003705 |
| inclination: | 69.9984° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 151.0029° |
| argument of perigee: | 267.4567° |
| revolutions per day: | 14.98330638 |
| mean anomaly at epoch: | 92.6168° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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