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 27431U 26138.13633766 +.00000000 +00000-0 +68472-4 0 00006
2 27431 98.9540 188.6004 0014782 331.0464 28.9885 14.10220108 03
| Epoch (UTC): | 18 May 2026 03:16:19 |
| Eccentricity: | 0.0014782 |
| inclination: | 98.9540° |
| perigee height: | 848 km |
| apogee height: | 869 km |
| right ascension of ascending node: | 188.6004° |
| argument of perigee: | 331.0464° |
| revolutions per day: | 14.10220108 |
| mean anomaly at epoch: | 28.9885° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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