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 36792U 26145.56024166 +.00000000 +00000-0 +00000-0 0 00008
2 36792 0.0397 89.3856 0001910 317.5784 279.0688 1.00272392 09
| Epoch (UTC): | 25 May 2026 13:26:44 |
| Eccentricity: | 0.0001910 |
| inclination: | 0.0397° |
| perigee height: | 35778 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 89.3856° |
| argument of perigee: | 317.5784° |
| revolutions per day: | 1.00272392 |
| mean anomaly at epoch: | 279.0688° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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