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 38095U 26100.69470138 +.00000000 +00000-0 +26604-2 0 00005
2 38095 20.9801 47.3815 6569907 0.7988 359.7900 3.25149935 03
| Epoch (UTC): | 10 April 2026 16:40:22 |
| Eccentricity: | 0.6569907 |
| inclination: | 20.9801° |
| perigee height: | 224 km |
| apogee height: | 25513 km |
| right ascension of ascending node: | 47.3815° |
| argument of perigee: | 0.7988° |
| revolutions per day: | 3.25149935 |
| mean anomaly at epoch: | 359.7900° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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