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 26087.89958895 +.00000000 +00000-0 +73988-4 0 00007
2 27598 98.8529 59.9752 0008383 205.6884 154.3882 14.29706970 02
| Epoch (UTC): | 28 March 2026 21:35:24 |
| Eccentricity: | 0.0008383 |
| inclination: | 98.8529° |
| perigee height: | 787 km |
| apogee height: | 799 km |
| right ascension of ascending node: | 59.9752° |
| argument of perigee: | 205.6884° |
| revolutions per day: | 14.29706970 |
| mean anomaly at epoch: | 154.3882° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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