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 43657U 26145.38154146 +.00000000 +00000-0 +42395-4 0 00005
2 43657 67.1466 133.1864 0007719 281.7547 78.2672 13.96707651 08
| Epoch (UTC): | 25 May 2026 09:09:25 |
| Eccentricity: | 0.0007719 |
| inclination: | 67.1466° |
| perigee height: | 900 km |
| apogee height: | 911 km |
| right ascension of ascending node: | 133.1864° |
| argument of perigee: | 281.7547° |
| revolutions per day: | 13.96707651 |
| mean anomaly at epoch: | 78.2672° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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