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 63518U 26145.28681463 +.00000000 +00000-0 +58315-3 0 00007
2 63518 53.1578 143.6457 0000946 68.1967 291.9139 15.42179789 07
| Epoch (UTC): | 25 May 2026 06:53:00 |
| Eccentricity: | 0.0000946 |
| inclination: | 53.1578° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 143.6457° |
| argument of perigee: | 68.1967° |
| revolutions per day: | 15.42179789 |
| mean anomaly at epoch: | 291.9139° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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