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 18009U 26146.13890547 +.00000000 +00000-0 +64329-3 0 00004
2 18009 63.2945 59.3882 0784521 104.8604 264.0618 13.86838454 01
| Epoch (UTC): | 26 May 2026 03:20:01 |
| Eccentricity: | 0.0784521 |
| inclination: | 63.2945° |
| perigee height: | 366 km |
| apogee height: | 1514 km |
| right ascension of ascending node: | 59.3882° |
| argument of perigee: | 104.8604° |
| revolutions per day: | 13.86838454 |
| mean anomaly at epoch: | 264.0618° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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