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 43233U 26145.39842719 +.00000000 +00000-0 +00000-0 0 00009
2 43233 0.0486 8.4640 0002880 55.9511 295.6141 5.00115729 09
| Epoch (UTC): | 25 May 2026 09:33:44 |
| Eccentricity: | 0.0002880 |
| inclination: | 0.0486° |
| perigee height: | 8062 km |
| apogee height: | 8070 km |
| right ascension of ascending node: | 8.4640° |
| argument of perigee: | 55.9511° |
| revolutions per day: | 5.00115729 |
| mean anomaly at epoch: | 295.6141° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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