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 23406U 26088.05745972 +.00000000 +00000-0 +11280-3 0 00006
2 23406 71.0312 208.1294 0199805 31.8411 148.0046 13.73443795 06
| Epoch (UTC): | 29 March 2026 01:22:44 |
| Eccentricity: | 0.0199805 |
| inclination: | 71.0312° |
| perigee height: | 840 km |
| apogee height: | 1134 km |
| right ascension of ascending node: | 208.1294° |
| argument of perigee: | 31.8411° |
| revolutions per day: | 13.73443795 |
| mean anomaly at epoch: | 148.0046° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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