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 27646U 26070.82601029 +.00000000 +00000-0 +27194-3 0 00007
2 27646 49.5191 266.5746 5410806 126.1702 352.5845 4.61717959 06
| Epoch (UTC): | 11 March 2026 19:49:27 |
| Eccentricity: | 0.5410806 |
| inclination: | 49.5191° |
| perigee height: | 613 km |
| apogee height: | 17099 km |
| right ascension of ascending node: | 266.5746° |
| argument of perigee: | 126.1702° |
| revolutions per day: | 4.61717959 |
| mean anomaly at epoch: | 352.5845° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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