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 43805U 26106.20265466 +.00000000 +00000-0 +10531-2 0 00001
2 43805 97.3995 184.5900 0003944 232.6201 127.4711 15.86191538 07
| Epoch (UTC): | 16 April 2026 04:51:49 |
| Eccentricity: | 0.0003944 |
| inclination: | 97.3995° |
| perigee height: | 310 km |
| apogee height: | 316 km |
| right ascension of ascending node: | 184.5900° |
| argument of perigee: | 232.6201° |
| revolutions per day: | 15.86191538 |
| mean anomaly at epoch: | 127.4711° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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