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 45863U 26145.53904600 +.00000000 +00000-0 +00000-0 0 00004
2 45863 0.0454 104.3287 0002381 357.0931 109.8259 1.00265446 00
| Epoch (UTC): | 25 May 2026 12:56:13 |
| Eccentricity: | 0.0002381 |
| inclination: | 0.0454° |
| perigee height: | 35778 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 104.3287° |
| argument of perigee: | 357.0931° |
| revolutions per day: | 1.00265446 |
| mean anomaly at epoch: | 109.8259° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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