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 39643U 26030.72964779 +.00000000 +00000-0 +25661-3 0 00003
2 39643 65.0105 29.6299 0015386 279.2229 80.7117 14.34596989 09
| Epoch (UTC): | 30 January 2026 17:30:41 |
| Eccentricity: | 0.0015386 |
| inclination: | 65.0105° |
| perigee height: | 765 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 29.6299° |
| argument of perigee: | 279.2229° |
| revolutions per day: | 14.34596989 |
| mean anomaly at epoch: | 80.7117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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