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 63459U 26145.37529272 +.00000000 +00000-0 +27510-3 0 00003
2 63459 53.1589 143.5605 0001207 94.6334 265.4810 15.42165062 01
| Epoch (UTC): | 25 May 2026 09:00:25 |
| Eccentricity: | 0.0001207 |
| inclination: | 53.1589° |
| perigee height: | 439 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 143.5605° |
| argument of perigee: | 94.6334° |
| revolutions per day: | 15.42165062 |
| mean anomaly at epoch: | 265.4810° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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