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 26018.59541624 +.00000000 +00000-0 +10314-3 0 00002
2 23405 70.9835 97.8807 0004823 255.6940 104.3647 14.15557014 03
| Epoch (UTC): | 18 January 2026 14:17:23 |
| Eccentricity: | 0.0004823 |
| inclination: | 70.9835° |
| perigee height: | 837 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 97.8807° |
| argument of perigee: | 255.6940° |
| revolutions per day: | 14.15557014 |
| mean anomaly at epoch: | 104.3647° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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