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 63926U 26145.22483228 +.00000000 +00000-0 +30328-3 0 00007
2 63926 70.0012 81.6111 0003117 266.8666 93.2136 14.98337583 03
| Epoch (UTC): | 25 May 2026 05:23:45 |
| Eccentricity: | 0.0003117 |
| inclination: | 70.0012° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 81.6111° |
| argument of perigee: | 266.8666° |
| revolutions per day: | 14.98337583 |
| mean anomaly at epoch: | 93.2136° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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