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 63479U 26145.54902265 +.00000000 +00000-0 +29370-3 0 00007
2 63479 43.0000 182.0356 0001269 276.1874 83.8833 15.27585022 06
| Epoch (UTC): | 25 May 2026 13:10:35 |
| Eccentricity: | 0.0001269 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 182.0356° |
| argument of perigee: | 276.1874° |
| revolutions per day: | 15.27585022 |
| mean anomaly at epoch: | 83.8833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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