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 55009U 26145.59164300 +.00000000 +00000-0 +33625-3 0 00000
2 55009 97.3185 209.9742 0005937 178.8238 181.3024 15.41904847 00
| Epoch (UTC): | 25 May 2026 14:11:57 |
| Eccentricity: | 0.0005937 |
| inclination: | 97.3185° |
| perigee height: | 436 km |
| apogee height: | 445 km |
| right ascension of ascending node: | 209.9742° |
| argument of perigee: | 178.8238° |
| revolutions per day: | 15.41904847 |
| mean anomaly at epoch: | 181.3024° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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