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 43005U 26145.65279669 +.00000000 +00000-0 +13680-3 0 00004
2 43005 97.9559 218.2933 0001680 100.4687 259.6713 14.77105155 06
| Epoch (UTC): | 25 May 2026 15:40:01 |
| Eccentricity: | 0.0001680 |
| inclination: | 97.9559° |
| perigee height: | 637 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 218.2933° |
| argument of perigee: | 100.4687° |
| revolutions per day: | 14.77105155 |
| mean anomaly at epoch: | 259.6713° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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