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 39440U 26073.79119559 +.00000000 +00000-0 +71207-3 0 00007
2 39440 97.8811 22.4718 0057976 342.0979 17.8197 14.93025936 03
| Epoch (UTC): | 14 March 2026 18:59:19 |
| Eccentricity: | 0.0057976 |
| inclination: | 97.8811° |
| perigee height: | 548 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 22.4718° |
| argument of perigee: | 342.0979° |
| revolutions per day: | 14.93025936 |
| mean anomaly at epoch: | 17.8197° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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