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 43562U 26145.35735713 +.00000000 +00000-0 +00000-0 0 00005
2 43562 0.0357 154.0869 0002360 307.8827 206.6203 1.00271166 09
| Epoch (UTC): | 25 May 2026 08:34:35 |
| Eccentricity: | 0.0002360 |
| inclination: | 0.0357° |
| perigee height: | 35777 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 154.0869° |
| argument of perigee: | 307.8827° |
| revolutions per day: | 1.00271166 |
| mean anomaly at epoch: | 206.6203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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