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 26073.47836869 +.00000000 +00000-0 -73240-4 0 00006
2 23404 71.0131 89.1096 0016874 331.0958 28.9228 14.13931973 08
| Epoch (UTC): | 14 March 2026 11:28:51 |
| Eccentricity: | 0.0016874 |
| inclination: | 71.0131° |
| perigee height: | 834 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 89.1096° |
| argument of perigee: | 331.0958° |
| revolutions per day: | 14.13931973 |
| mean anomaly at epoch: | 28.9228° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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