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 39679U 26065.51232791 +.00000000 +00000-0 +41192-3 0 00006
2 39679 51.6093 352.7772 0097822 91.4081 269.8112 15.39057855 01
| Epoch (UTC): | 06 March 2026 12:17:45 |
| Eccentricity: | 0.0097822 |
| inclination: | 51.6093° |
| perigee height: | 382 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 352.7772° |
| argument of perigee: | 91.4081° |
| revolutions per day: | 15.39057855 |
| mean anomaly at epoch: | 269.8112° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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