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 26106.97856435 +.00000000 +00000-0 +30336-4 0 00000
2 40336 98.3412 165.7512 0000936 136.9911 223.1349 14.35542598 00
| Epoch (UTC): | 16 April 2026 23:29:07 |
| Eccentricity: | 0.0000936 |
| inclination: | 98.3412° |
| perigee height: | 773 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 165.7512° |
| argument of perigee: | 136.9911° |
| revolutions per day: | 14.35542598 |
| mean anomaly at epoch: | 223.1349° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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