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 26039.44146922 +.00000000 +00000-0 +80567-4 0 00009
2 23405 70.9815 54.0215 0004302 236.3068 123.7645 14.15557113 01
| Epoch (UTC): | 08 February 2026 10:35:42 |
| Eccentricity: | 0.0004302 |
| inclination: | 70.9815° |
| perigee height: | 837 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 54.0215° |
| argument of perigee: | 236.3068° |
| revolutions per day: | 14.15557113 |
| mean anomaly at epoch: | 123.7645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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