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 27387U 26044.92505564 +.00000000 +00000-0 +45855-4 0 00003
2 27387 98.8165 60.1682 0032965 128.8509 231.5626 14.36764267 08
| Epoch (UTC): | 13 February 2026 22:12:04 |
| Eccentricity: | 0.0032965 |
| inclination: | 98.8165° |
| perigee height: | 746 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 60.1682° |
| argument of perigee: | 128.8509° |
| revolutions per day: | 14.36764267 |
| mean anomaly at epoch: | 231.5626° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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