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 26138.81566816 +.00000000 +00000-0 +00000-0 0 00008
2 43700 0.0148 324.5139 0001252 123.5484 107.8717 1.00269597 03
| Epoch (UTC): | 18 May 2026 19:34:33 |
| Eccentricity: | 0.0001252 |
| inclination: | 0.0148° |
| perigee height: | 35782 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 324.5139° |
| argument of perigee: | 123.5484° |
| revolutions per day: | 1.00269597 |
| mean anomaly at epoch: | 107.8717° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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