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 43271U 26145.61711272 +.00000000 +00000-0 +00000-0 0 00005
2 43271 0.0141 290.8058 0001066 147.9551 188.5999 1.00271179 09
| Epoch (UTC): | 25 May 2026 14:48:38 |
| Eccentricity: | 0.0001066 |
| inclination: | 0.0141° |
| perigee height: | 35782 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 290.8058° |
| argument of perigee: | 147.9551° |
| revolutions per day: | 1.00271179 |
| mean anomaly at epoch: | 188.5999° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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