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 63931U 26145.54210279 +.00000000 +00000-0 +26149-3 0 00008
2 63931 70.0014 80.7071 0002222 274.8537 85.2368 14.98333395 03
| Epoch (UTC): | 25 May 2026 13:00:37 |
| Eccentricity: | 0.0002222 |
| inclination: | 70.0014° |
| perigee height: | 571 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 80.7071° |
| argument of perigee: | 274.8537° |
| revolutions per day: | 14.98333395 |
| mean anomaly at epoch: | 85.2368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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