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 26138.50035353 +.00000000 +00000-0 +25742-4 0 00007
2 27386 98.3820 90.4840 0001219 91.7123 21.4364 14.39057015 04
| Epoch (UTC): | 18 May 2026 12:00:30 |
| Eccentricity: | 0.0001219 |
| inclination: | 98.3820° |
| perigee height: | 761 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 90.4840° |
| argument of perigee: | 91.7123° |
| revolutions per day: | 14.39057015 |
| mean anomaly at epoch: | 21.4364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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