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 59738U 26145.34657080 +.00000000 +00000-0 +37250-4 0 00007
2 59738 43.0030 110.5912 0000874 273.0709 87.0043 15.27576758 05
| Epoch (UTC): | 25 May 2026 08:19:03 |
| Eccentricity: | 0.0000874 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 110.5912° |
| argument of perigee: | 273.0709° |
| revolutions per day: | 15.27576758 |
| mean anomaly at epoch: | 87.0043° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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