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 40272U 26145.49823830 +.00000000 +00000-0 +00000-0 0 00003
2 40272 0.0498 76.5753 0001838 337.6402 296.4286 1.00271173 05
| Epoch (UTC): | 25 May 2026 11:57:27 |
| Eccentricity: | 0.0001838 |
| inclination: | 0.0498° |
| perigee height: | 35779 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 76.5753° |
| argument of perigee: | 337.6402° |
| revolutions per day: | 1.00271173 |
| mean anomaly at epoch: | 296.4286° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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