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 23705U 26105.38000727 +.00000000 +00000-0 +16690-3 0 00006
2 23705 71.0192 103.2242 0010616 58.3866 301.8292 14.15502911 07
| Epoch (UTC): | 15 April 2026 09:07:12 |
| Eccentricity: | 0.0010616 |
| inclination: | 71.0192° |
| perigee height: | 833 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 103.2242° |
| argument of perigee: | 58.3866° |
| revolutions per day: | 14.15502911 |
| mean anomaly at epoch: | 301.8292° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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