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 63957U 26145.25521470 +.00000000 +00000-0 +55491-3 0 00004
2 63957 43.0010 104.0260 0001014 270.6230 89.4506 15.27586901 05
| Epoch (UTC): | 25 May 2026 06:07:30 |
| Eccentricity: | 0.0001014 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 104.0260° |
| argument of perigee: | 270.6230° |
| revolutions per day: | 15.27586901 |
| mean anomaly at epoch: | 89.4506° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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