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 43655U 26145.60346553 +.00000000 +00000-0 +48818-4 0 00009
2 43655 99.3296 154.7009 0001300 35.3441 324.7797 13.79306921 03
| Epoch (UTC): | 25 May 2026 14:28:59 |
| Eccentricity: | 0.0001300 |
| inclination: | 99.3296° |
| perigee height: | 965 km |
| apogee height: | 967 km |
| right ascension of ascending node: | 154.7009° |
| argument of perigee: | 35.3441° |
| revolutions per day: | 13.79306921 |
| mean anomaly at epoch: | 324.7797° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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