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 38740U 26145.38335727 +.00000000 +00000-0 +00000-0 0 00001
2 38740 0.0046 145.5359 0001686 33.6660 270.2831 1.00272060 02
| Epoch (UTC): | 25 May 2026 09:12:02 |
| Eccentricity: | 0.0001686 |
| inclination: | 0.0046° |
| perigee height: | 35779 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 145.5359° |
| argument of perigee: | 33.6660° |
| revolutions per day: | 1.00272060 |
| mean anomaly at epoch: | 270.2831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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