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 23404U 26064.56440324 +.00000000 +00000-0 +34859-4 0 00005
2 23404 71.0138 107.7839 0016171 344.5433 15.5193 14.13933029 01
| Epoch (UTC): | 05 March 2026 13:32:44 |
| Eccentricity: | 0.0016171 |
| inclination: | 71.0138° |
| perigee height: | 834 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 107.7839° |
| argument of perigee: | 344.5433° |
| revolutions per day: | 14.13933029 |
| mean anomaly at epoch: | 15.5193° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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