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 26135.30411144 +.00000000 +00000-0 +22458-4 0 00009
2 27386 98.3818 87.3599 0001211 91.7971 32.4733 14.39056527 09
| Epoch (UTC): | 15 May 2026 07:17:55 |
| Eccentricity: | 0.0001211 |
| inclination: | 98.3818° |
| perigee height: | 761 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 87.3599° |
| argument of perigee: | 91.7971° |
| revolutions per day: | 14.39056527 |
| mean anomaly at epoch: | 32.4733° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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