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 38779U 26145.52891845 +.00000000 +00000-0 +00000-0 0 00007
2 38779 0.0438 261.2985 0007665 182.5549 72.6543 1.00273170 00
| Epoch (UTC): | 25 May 2026 12:41:38 |
| Eccentricity: | 0.0007665 |
| inclination: | 0.0438° |
| perigee height: | 35754 km |
| apogee height: | 35819 km |
| right ascension of ascending node: | 261.2985° |
| argument of perigee: | 182.5549° |
| revolutions per day: | 1.00273170 |
| mean anomaly at epoch: | 72.6543° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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