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 26110.38910884 +.00000000 +00000-0 +19405-3 0 00002
2 39446 97.8660 66.1141 0049918 150.8479 209.5545 14.96551872 06
| Epoch (UTC): | 20 April 2026 09:20:19 |
| Eccentricity: | 0.0049918 |
| inclination: | 97.8660° |
| perigee height: | 543 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 66.1141° |
| argument of perigee: | 150.8479° |
| revolutions per day: | 14.96551872 |
| mean anomaly at epoch: | 209.5545° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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