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 26101.44021100 +.00000000 +00000-0 +40024-4 0 00005
2 27386 98.3779 54.2690 0001166 83.2856 27.5991 14.39048790 01
| Epoch (UTC): | 11 April 2026 10:33:54 |
| Eccentricity: | 0.0001166 |
| inclination: | 98.3779° |
| perigee height: | 761 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 54.2690° |
| argument of perigee: | 83.2856° |
| revolutions per day: | 14.39048790 |
| mean anomaly at epoch: | 27.5991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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