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 40336U 26076.93815440 +.00000000 +00000-0 -39279-4 0 00009
2 40336 98.3471 136.6853 0000599 43.6139 316.5095 14.35516804 07
| Epoch (UTC): | 17 March 2026 22:30:56 |
| Eccentricity: | 0.0000599 |
| inclination: | 98.3471° |
| perigee height: | 773 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 136.6853° |
| argument of perigee: | 43.6139° |
| revolutions per day: | 14.35516804 |
| mean anomaly at epoch: | 316.5095° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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