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 40072U 26145.32901854 +.00000000 +00000-0 +13671-3 0 00007
2 40072 98.3825 102.9943 0005659 7.3346 352.7951 14.87956954 06
| Epoch (UTC): | 25 May 2026 07:53:47 |
| Eccentricity: | 0.0005659 |
| inclination: | 98.3825° |
| perigee height: | 600 km |
| apogee height: | 608 km |
| right ascension of ascending node: | 102.9943° |
| argument of perigee: | 7.3346° |
| revolutions per day: | 14.87956954 |
| mean anomaly at epoch: | 352.7951° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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