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 26145.10043962 +.00000000 +00000-0 +00000-0 0 00009
2 22009 14.2063 9.8448 0007889 27.5092 320.6798 0.98809616 03
| Epoch (UTC): | 25 May 2026 02:24:37 |
| Eccentricity: | 0.0007889 |
| inclination: | 14.2063° |
| perigee height: | 36168 km |
| apogee height: | 36235 km |
| right ascension of ascending node: | 9.8448° |
| argument of perigee: | 27.5092° |
| revolutions per day: | 0.98809616 |
| mean anomaly at epoch: | 320.6798° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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