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 63469U 26145.42420868 +.00000000 +00000-0 +20243-3 0 00007
2 63469 43.0110 186.2978 0003990 287.3298 72.7117 15.27560993 02
| Epoch (UTC): | 25 May 2026 10:10:51 |
| Eccentricity: | 0.0003990 |
| inclination: | 43.0110° |
| perigee height: | 480 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 186.2978° |
| argument of perigee: | 287.3298° |
| revolutions per day: | 15.27560993 |
| mean anomaly at epoch: | 72.7117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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