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 26133.42777407 +.00000000 +00000-0 +15075-3 0 00007
2 39440 97.8890 82.2722 0058866 141.3076 219.2383 14.93493448 08
| Epoch (UTC): | 13 May 2026 10:15:59 |
| Eccentricity: | 0.0058866 |
| inclination: | 97.8890° |
| perigee height: | 546 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 82.2722° |
| argument of perigee: | 141.3076° |
| revolutions per day: | 14.93493448 |
| mean anomaly at epoch: | 219.2383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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