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 26017.36760159 +.00000000 +00000-0 +00000-0 0 00004
2 42075 0.0237 42.3379 0000536 339.2520 215.5624 1.00271462 06
| Epoch (UTC): | 17 January 2026 08:49:20 |
| Eccentricity: | 0.0000536 |
| inclination: | 0.0237° |
| perigee height: | 35784 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 42.3379° |
| argument of perigee: | 339.2520° |
| revolutions per day: | 1.00271462 |
| mean anomaly at epoch: | 215.5624° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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