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 26066.85712159 +.00000000 +00000-0 +69788-3 0 00008
2 39446 97.8591 22.3820 0048608 298.5601 61.0732 14.96154402 06
| Epoch (UTC): | 07 March 2026 20:34:15 |
| Eccentricity: | 0.0048608 |
| inclination: | 97.8591° |
| perigee height: | 545 km |
| apogee height: | 613 km |
| right ascension of ascending node: | 22.3820° |
| argument of perigee: | 298.5601° |
| revolutions per day: | 14.96154402 |
| mean anomaly at epoch: | 61.0732° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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