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 26150.79569052 +.00000000 +00000-0 +57773-3 0 00009
2 23606 98.3146 5.5650 0004418 298.4483 61.6312 15.34618498 04
| Epoch (UTC): | 30 May 2026 19:05:47 |
| Eccentricity: | 0.0004418 |
| inclination: | 98.3146° |
| perigee height: | 459 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 5.5650° |
| argument of perigee: | 298.4483° |
| revolutions per day: | 15.34618498 |
| mean anomaly at epoch: | 61.6312° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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