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 63941U 26145.52957816 +.00000000 +00000-0 -33367-5 0 00005
2 63941 70.0006 80.6546 0003289 268.5281 91.5502 14.98330820 01
| Epoch (UTC): | 25 May 2026 12:42:35 |
| Eccentricity: | 0.0003289 |
| inclination: | 70.0006° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 80.6546° |
| argument of perigee: | 268.5281° |
| revolutions per day: | 14.98330820 |
| mean anomaly at epoch: | 91.5502° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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