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 42075U 26146.22305608 +.00000000 +00000-0 +00000-0 0 00006
2 42075 0.0144 275.6061 0000218 97.8831 298.5991 1.00271756 05
| Epoch (UTC): | 26 May 2026 05:21:12 |
| Eccentricity: | 0.0000218 |
| inclination: | 0.0144° |
| perigee height: | 35786 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 275.6061° |
| argument of perigee: | 97.8831° |
| revolutions per day: | 1.00271756 |
| mean anomaly at epoch: | 298.5991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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