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 37792U 26134.09163895 +.00000000 +00000-0 +75346-4 0 00007
2 37792 98.2446 66.1706 0053556 111.9230 248.7687 14.81000082 06
| Epoch (UTC): | 14 May 2026 02:11:57 |
| Eccentricity: | 0.0053556 |
| inclination: | 98.2446° |
| perigee height: | 589 km |
| apogee height: | 664 km |
| right ascension of ascending node: | 66.1706° |
| argument of perigee: | 111.9230° |
| revolutions per day: | 14.81000082 |
| mean anomaly at epoch: | 248.7687° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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