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 62457U 26145.49598498 +.00000000 +00000-0 +00000-0 0 00001
2 62457 0.0685 138.8702 0001800 327.9612 231.6939 1.00271679 09
| Epoch (UTC): | 25 May 2026 11:54:13 |
| Eccentricity: | 0.0001800 |
| inclination: | 0.0685° |
| perigee height: | 35779 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 138.8702° |
| argument of perigee: | 327.9612° |
| revolutions per day: | 1.00271679 |
| mean anomaly at epoch: | 231.6939° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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