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 42749U 26145.58580845 +.00000000 +00000-0 +00000-0 0 00000
2 42749 1.7735 354.2812 0002371 68.2908 41.7347 1.00271715 02
| Epoch (UTC): | 25 May 2026 14:03:33 |
| Eccentricity: | 0.0002371 |
| inclination: | 1.7735° |
| perigee height: | 35777 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 354.2812° |
| argument of perigee: | 68.2908° |
| revolutions per day: | 1.00271715 |
| mean anomaly at epoch: | 41.7347° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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