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 43689U 26145.54402735 +.00000000 +00000-0 +63709-4 0 00000
2 43689 98.6655 205.5600 0000799 150.8284 209.2938 14.21505074 04
| Epoch (UTC): | 25 May 2026 13:03:23 |
| Eccentricity: | 0.0000799 |
| inclination: | 98.6655° |
| perigee height: | 820 km |
| apogee height: | 821 km |
| right ascension of ascending node: | 205.5600° |
| argument of perigee: | 150.8284° |
| revolutions per day: | 14.21505074 |
| mean anomaly at epoch: | 209.2938° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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