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 23405U 26129.75027700 +.00000000 +00000-0 -82409-4 0 00003
2 23405 70.9829 224.0256 0000779 14.1039 346.0105 14.15569653 07
| Epoch (UTC): | 09 May 2026 18:00:23 |
| Eccentricity: | 0.0000779 |
| inclination: | 70.9829° |
| perigee height: | 840 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 224.0256° |
| argument of perigee: | 14.1039° |
| revolutions per day: | 14.15569653 |
| mean anomaly at epoch: | 346.0105° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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