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 39446U 26066.38896579 +.00000000 +00000-0 +70424-3 0 00004
2 39446 97.8593 21.9121 0048642 300.1835 59.4572 14.96147910 03
| Epoch (UTC): | 07 March 2026 09:20:06 |
| Eccentricity: | 0.0048642 |
| inclination: | 97.8593° |
| perigee height: | 545 km |
| apogee height: | 613 km |
| right ascension of ascending node: | 21.9121° |
| argument of perigee: | 300.1835° |
| revolutions per day: | 14.96147910 |
| mean anomaly at epoch: | 59.4572° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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