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 26111.18164231 +.00000000 +00000-0 +15978-2 0 00002
2 43805 97.3963 189.9952 0004658 238.7547 121.3270 15.89660860 06
| Epoch (UTC): | 21 April 2026 04:21:33 |
| Eccentricity: | 0.0004658 |
| inclination: | 97.3963° |
| perigee height: | 300 km |
| apogee height: | 306 km |
| right ascension of ascending node: | 189.9952° |
| argument of perigee: | 238.7547° |
| revolutions per day: | 15.89660860 |
| mean anomaly at epoch: | 121.3270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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