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 26069.96374227 +.00000000 +00000-0 +85798-3 0 00004
2 18009 63.2923 272.6035 0792526 103.3957 265.6612 13.85476387 09
| Epoch (UTC): | 10 March 2026 23:07:47 |
| Eccentricity: | 0.0792526 |
| inclination: | 63.2923° |
| perigee height: | 364 km |
| apogee height: | 1525 km |
| right ascension of ascending node: | 272.6035° |
| argument of perigee: | 103.3957° |
| revolutions per day: | 13.85476387 |
| mean anomaly at epoch: | 265.6612° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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