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 40056U 26118.63470064 +.00000000 +00000-0 +14079-3 0 00000
2 40056 98.3194 352.1549 0013018 165.0357 195.1242 14.81189089 03
| Epoch (UTC): | 28 April 2026 15:13:58 |
| Eccentricity: | 0.0013018 |
| inclination: | 98.3194° |
| perigee height: | 616 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 352.1549° |
| argument of perigee: | 165.0357° |
| revolutions per day: | 14.81189089 |
| mean anomaly at epoch: | 195.1242° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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