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 27598U 26106.86522353 +.00000000 +00000-0 +38698-4 0 00001
2 27598 98.8556 79.2546 0009408 150.3849 209.7867 14.29713874 03
| Epoch (UTC): | 16 April 2026 20:45:55 |
| Eccentricity: | 0.0009408 |
| inclination: | 98.8556° |
| perigee height: | 786 km |
| apogee height: | 799 km |
| right ascension of ascending node: | 79.2546° |
| argument of perigee: | 150.3849° |
| revolutions per day: | 14.29713874 |
| mean anomaly at epoch: | 209.7867° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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