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 26145.58884178 +.00000000 +00000-0 +00000-0 0 00004
2 43700 0.0389 94.9524 0001698 359.9892 26.0068 1.00273244 03
| Epoch (UTC): | 25 May 2026 14:07:55 |
| Eccentricity: | 0.0001698 |
| inclination: | 0.0389° |
| perigee height: | 35779 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 94.9524° |
| argument of perigee: | 359.9892° |
| revolutions per day: | 1.00273244 |
| mean anomaly at epoch: | 26.0068° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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