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 63509U 26145.43440764 +.00000000 +00000-0 +43102-3 0 00009
2 63509 53.1575 143.1467 0001162 94.3053 265.8081 15.31715467 01
| Epoch (UTC): | 25 May 2026 10:25:32 |
| Eccentricity: | 0.0001162 |
| inclination: | 53.1575° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 143.1467° |
| argument of perigee: | 94.3053° |
| revolutions per day: | 15.31715467 |
| mean anomaly at epoch: | 265.8081° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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