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 26071.40481442 +.00000000 +00000-0 +52829-3 0 00001
2 39446 97.8588 26.9469 0048200 282.7822 76.8015 14.96214975 09
| Epoch (UTC): | 12 March 2026 09:42:55 |
| Eccentricity: | 0.0048200 |
| inclination: | 97.8588° |
| perigee height: | 545 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 26.9469° |
| argument of perigee: | 282.7822° |
| revolutions per day: | 14.96214975 |
| mean anomaly at epoch: | 76.8015° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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