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 26050.32535068 +.00000000 +00000-0 +00000-0 0 00002
2 43700 0.0168 211.9216 0002492 156.3478 283.9329 1.00272865 01
| Epoch (UTC): | 19 February 2026 07:48:30 |
| Eccentricity: | 0.0002492 |
| inclination: | 0.0168° |
| perigee height: | 35776 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 211.9216° |
| argument of perigee: | 156.3478° |
| revolutions per day: | 1.00272865 |
| mean anomaly at epoch: | 283.9329° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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