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 63505U 26145.43625295 +.00000000 +00000-0 +20033-3 0 00007
2 63505 53.1582 143.1915 0001253 56.8756 303.2365 15.30198697 08
| Epoch (UTC): | 25 May 2026 10:28:12 |
| Eccentricity: | 0.0001253 |
| inclination: | 53.1582° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 143.1915° |
| argument of perigee: | 56.8756° |
| revolutions per day: | 15.30198697 |
| mean anomaly at epoch: | 303.2365° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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