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 26074.79647693 +.00000000 +00000-0 +51439-3 0 00008
2 39440 97.8815 23.4787 0057849 338.8041 21.0781 14.93035357 00
| Epoch (UTC): | 15 March 2026 19:06:55 |
| Eccentricity: | 0.0057849 |
| inclination: | 97.8815° |
| perigee height: | 548 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 23.4787° |
| argument of perigee: | 338.8041° |
| revolutions per day: | 14.93035357 |
| mean anomaly at epoch: | 21.0781° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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