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 26044.45865426 +.00000000 +00000-0 +19011-3 0 00008
2 23405 70.9823 43.4655 0004083 232.5966 127.4786 14.15559986 08
| Epoch (UTC): | 13 February 2026 11:00:27 |
| Eccentricity: | 0.0004083 |
| inclination: | 70.9823° |
| perigee height: | 837 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 43.4655° |
| argument of perigee: | 232.5966° |
| revolutions per day: | 14.15559986 |
| mean anomaly at epoch: | 127.4786° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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