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 26071.14375755 +.00000000 +00000-0 -53945-4 0 00000
2 23404 71.0132 94.0006 0016705 334.5299 25.4998 14.13932652 05
| Epoch (UTC): | 12 March 2026 03:27:00 |
| Eccentricity: | 0.0016705 |
| inclination: | 71.0132° |
| perigee height: | 834 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 94.0006° |
| argument of perigee: | 334.5299° |
| revolutions per day: | 14.13932652 |
| mean anomaly at epoch: | 25.4998° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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