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 37840U 26155.32117808 +.00000000 +00000-0 +41607-4 0 00006
2 37840 19.9605 122.9684 0013809 100.3979 259.7982 14.11435848 07
| Epoch (UTC): | 04 June 2026 07:42:29 |
| Eccentricity: | 0.0013809 |
| inclination: | 19.9605° |
| perigee height: | 844 km |
| apogee height: | 864 km |
| right ascension of ascending node: | 122.9684° |
| argument of perigee: | 100.3979° |
| revolutions per day: | 14.11435848 |
| mean anomaly at epoch: | 259.7982° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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