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 38775U 26145.27851961 +.00000000 +00000-0 +00000-0 0 00000
2 38775 56.5251 63.6515 0014121 353.6091 6.3653 1.86230864 09
| Epoch (UTC): | 25 May 2026 06:41:04 |
| Eccentricity: | 0.0014121 |
| inclination: | 56.5251° |
| perigee height: | 21489 km |
| apogee height: | 21567 km |
| right ascension of ascending node: | 63.6515° |
| argument of perigee: | 353.6091° |
| revolutions per day: | 1.86230864 |
| mean anomaly at epoch: | 6.3653° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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