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 23606U 26162.20487831 +.00000000 +00000-0 +39656-3 0 00002
2 23606 98.3145 18.4160 0004559 246.2110 113.8653 15.35001933 05
| Epoch (UTC): | 11 June 2026 04:55:01 |
| Eccentricity: | 0.0004559 |
| inclination: | 98.3145° |
| perigee height: | 458 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 18.4160° |
| argument of perigee: | 246.2110° |
| revolutions per day: | 15.35001933 |
| mean anomaly at epoch: | 113.8653° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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