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 26071.57954596 +.00000000 +00000-0 +59060-3 0 00002
2 39440 97.8804 20.2569 0058286 349.3600 10.6381 14.92994645 08
| Epoch (UTC): | 12 March 2026 13:54:32 |
| Eccentricity: | 0.0058286 |
| inclination: | 97.8804° |
| perigee height: | 548 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 20.2569° |
| argument of perigee: | 349.3600° |
| revolutions per day: | 14.92994645 |
| mean anomaly at epoch: | 10.6381° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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