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 26065.41335212 +.00000000 +00000-0 +20898-4 0 00007
2 23404 71.0138 106.0056 0016256 343.2144 16.8438 14.13933116 06
| Epoch (UTC): | 06 March 2026 09:55:13 |
| Eccentricity: | 0.0016256 |
| inclination: | 71.0138° |
| perigee height: | 834 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 106.0056° |
| argument of perigee: | 343.2144° |
| revolutions per day: | 14.13933116 |
| mean anomaly at epoch: | 16.8438° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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