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 42070U 26133.44153543 +.00000000 +00000-0 +00000-0 0 00000
2 42070 0.0154 270.5927 0001956 138.2825 231.3967 1.00270601 05
| Epoch (UTC): | 13 May 2026 10:35:48 |
| Eccentricity: | 0.0001956 |
| inclination: | 0.0154° |
| perigee height: | 35779 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 270.5927° |
| argument of perigee: | 138.2825° |
| revolutions per day: | 1.00270601 |
| mean anomaly at epoch: | 231.3967° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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