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 63432U 26145.49392605 +.00000000 +00000-0 +19855-3 0 00008
2 63432 42.9990 167.3251 0229349 103.1514 259.5020 14.86351622 03
| Epoch (UTC): | 25 May 2026 11:51:15 |
| Eccentricity: | 0.0229349 |
| inclination: | 42.9990° |
| perigee height: | 449 km |
| apogee height: | 770 km |
| right ascension of ascending node: | 167.3251° |
| argument of perigee: | 103.1514° |
| revolutions per day: | 14.86351622 |
| mean anomaly at epoch: | 259.5020° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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