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 43700U 26111.86450859 +.00000000 +00000-0 +00000-0 0 00003
2 43700 0.0122 222.5816 0001060 182.1900 142.1503 1.00271924 07
| Epoch (UTC): | 21 April 2026 20:44:53 |
| Eccentricity: | 0.0001060 |
| inclination: | 0.0122° |
| perigee height: | 35782 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 222.5816° |
| argument of perigee: | 182.1900° |
| revolutions per day: | 1.00271924 |
| mean anomaly at epoch: | 142.1503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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