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 45026U 26145.52891845 +.00000000 +00000-0 +00000-0 0 00000
2 45026 0.0144 121.0716 0003426 312.2779 83.1960 1.00272127 01
| Epoch (UTC): | 25 May 2026 12:41:38 |
| Eccentricity: | 0.0003426 |
| inclination: | 0.0144° |
| perigee height: | 35772 km |
| apogee height: | 35801 km |
| right ascension of ascending node: | 121.0716° |
| argument of perigee: | 312.2779° |
| revolutions per day: | 1.00272127 |
| mean anomaly at epoch: | 83.1960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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