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 42934U 26145.50040500 +.00000000 +00000-0 +00000-0 0 00007
2 42934 0.0321 321.4374 0003215 55.7818 345.0194 1.00270769 07
| Epoch (UTC): | 25 May 2026 12:00:34 |
| Eccentricity: | 0.0003215 |
| inclination: | 0.0321° |
| perigee height: | 35773 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 321.4374° |
| argument of perigee: | 55.7818° |
| revolutions per day: | 1.00270769 |
| mean anomaly at epoch: | 345.0194° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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