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 42917U 26145.39505729 +.00000000 +00000-0 +00000-0 0 00004
2 42917 0.0894 121.2605 0002067 300.4945 90.4280 1.00267236 03
| Epoch (UTC): | 25 May 2026 09:28:52 |
| Eccentricity: | 0.0002067 |
| inclination: | 0.0894° |
| perigee height: | 35779 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 121.2605° |
| argument of perigee: | 300.4945° |
| revolutions per day: | 1.00267236 |
| mean anomaly at epoch: | 90.4280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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