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 68184U 26145.33940208 +.00000000 +00000-0 +10014-2 0 00005
2 68184 53.1591 270.3609 0001010 78.5002 281.6116 15.39003569 00
| Epoch (UTC): | 25 May 2026 08:08:44 |
| Eccentricity: | 0.0001010 |
| inclination: | 53.1591° |
| perigee height: | 448 km |
| apogee height: | 450 km |
| right ascension of ascending node: | 270.3609° |
| argument of perigee: | 78.5002° |
| revolutions per day: | 15.39003569 |
| mean anomaly at epoch: | 281.6116° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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