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 40403U 26101.50661117 +.00000000 +00000-0 +65837-3 0 00003
2 40403 98.6713 129.0735 0011796 210.5679 149.4818 14.30956634 04
| Epoch (UTC): | 11 April 2026 12:09:31 |
| Eccentricity: | 0.0011796 |
| inclination: | 98.6713° |
| perigee height: | 780 km |
| apogee height: | 797 km |
| right ascension of ascending node: | 129.0735° |
| argument of perigee: | 210.5679° |
| revolutions per day: | 14.30956634 |
| mean anomaly at epoch: | 149.4818° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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