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 23318U 26139.93771808 +.00000000 +00000-0 +25720-4 0 00004
2 23318 82.5423 23.9816 0022849 2.5578 357.5748 14.80945069 09
| Epoch (UTC): | 19 May 2026 22:30:18 |
| Eccentricity: | 0.0022849 |
| inclination: | 82.5423° |
| perigee height: | 610 km |
| apogee height: | 642 km |
| right ascension of ascending node: | 23.9816° |
| argument of perigee: | 2.5578° |
| revolutions per day: | 14.80945069 |
| mean anomaly at epoch: | 357.5748° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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