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 42741U 26145.26132573 +.00000000 +00000-0 +00000-0 0 00008
2 42741 0.0353 146.9701 0000117 185.9832 175.9738 1.00271623 06
| Epoch (UTC): | 25 May 2026 06:16:18 |
| Eccentricity: | 0.0000117 |
| inclination: | 0.0353° |
| perigee height: | 35786 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 146.9701° |
| argument of perigee: | 185.9832° |
| revolutions per day: | 1.00271623 |
| mean anomaly at epoch: | 175.9738° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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