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 26104.30171042 +.00000000 +00000-0 +28555-4 0 00009
2 27386 98.3783 57.0644 0001159 83.8694 82.6493 14.39049336 00
| Epoch (UTC): | 14 April 2026 07:14:27 |
| Eccentricity: | 0.0001159 |
| inclination: | 98.3783° |
| perigee height: | 761 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 57.0644° |
| argument of perigee: | 83.8694° |
| revolutions per day: | 14.39049336 |
| mean anomaly at epoch: | 82.6493° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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