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 22009U 26140.54232925 +.00000000 +00000-0 +00000-0 0 00001
2 22009 14.2034 9.8764 0007576 25.8656 140.8863 0.98810144 05
| Epoch (UTC): | 20 May 2026 13:00:57 |
| Eccentricity: | 0.0007576 |
| inclination: | 14.2034° |
| perigee height: | 36169 km |
| apogee height: | 36234 km |
| right ascension of ascending node: | 9.8764° |
| argument of perigee: | 25.8656° |
| revolutions per day: | 0.98810144 |
| mean anomaly at epoch: | 140.8863° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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