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 26065.79928338 +.00000000 +00000-0 -64101-4 0 00002
2 23405 70.9853 358.5692 0003268 216.0925 143.9978 14.15561386 01
| Epoch (UTC): | 06 March 2026 19:10:58 |
| Eccentricity: | 0.0003268 |
| inclination: | 70.9853° |
| perigee height: | 838 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 358.5692° |
| argument of perigee: | 216.0925° |
| revolutions per day: | 14.15561386 |
| mean anomaly at epoch: | 143.9978° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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