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 27386U 26105.87130446 +.00000000 +00000-0 +24832-4 0 00009
2 27386 98.3786 58.5978 0001157 84.3003 288.9145 14.39049572 04
| Epoch (UTC): | 15 April 2026 20:54:40 |
| Eccentricity: | 0.0001157 |
| inclination: | 98.3786° |
| perigee height: | 761 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 58.5978° |
| argument of perigee: | 84.3003° |
| revolutions per day: | 14.39049572 |
| mean anomaly at epoch: | 288.9145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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