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 26107.88788219 +.00000000 +00000-0 +27085-4 0 00002
2 27386 98.3788 60.5679 0001138 84.6613 289.5440 14.39049903 09
| Epoch (UTC): | 17 April 2026 21:18:33 |
| Eccentricity: | 0.0001138 |
| inclination: | 98.3788° |
| perigee height: | 761 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 60.5679° |
| argument of perigee: | 84.6613° |
| revolutions per day: | 14.39049903 |
| mean anomaly at epoch: | 289.5440° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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