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 38745U 26106.68990933 +.00000000 +00000-0 +42781-3 0 00007
2 38745 49.8246 262.6212 1586866 6.0129 355.7505 12.39246070 05
| Epoch (UTC): | 16 April 2026 16:33:28 |
| Eccentricity: | 0.1586866 |
| inclination: | 49.8246° |
| perigee height: | 258 km |
| apogee height: | 2762 km |
| right ascension of ascending node: | 262.6212° |
| argument of perigee: | 6.0129° |
| revolutions per day: | 12.39246070 |
| mean anomaly at epoch: | 355.7505° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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