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 63679U 26145.47460623 +.00000000 +00000-0 +54809-3 0 00003
2 63679 43.0013 317.2361 0001568 257.3975 102.6701 15.27578725 01
| Epoch (UTC): | 25 May 2026 11:23:25 |
| Eccentricity: | 0.0001568 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 317.2361° |
| argument of perigee: | 257.3975° |
| revolutions per day: | 15.27578725 |
| mean anomaly at epoch: | 102.6701° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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