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 43081U 26145.62898075 +.00000000 +00000-0 +18952-3 0 00000
2 43081 34.9962 287.5349 0005433 309.6199 50.4030 15.02572774 03
| Epoch (UTC): | 25 May 2026 15:05:43 |
| Eccentricity: | 0.0005433 |
| inclination: | 34.9962° |
| perigee height: | 555 km |
| apogee height: | 563 km |
| right ascension of ascending node: | 287.5349° |
| argument of perigee: | 309.6199° |
| revolutions per day: | 15.02572774 |
| mean anomaly at epoch: | 50.4030° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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