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 37779U 26110.58353646 +.00000000 +00000-0 +00000-0 0 00006
2 37779 0.5396 84.9398 0002772 317.9044 53.8606 1.00271658 03
| Epoch (UTC): | 20 April 2026 14:00:17 |
| Eccentricity: | 0.0002772 |
| inclination: | 0.5396° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 84.9398° |
| argument of perigee: | 317.9044° |
| revolutions per day: | 1.00271658 |
| mean anomaly at epoch: | 53.8606° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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