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 26144.81999302 +.00000000 +00000-0 +38651-3 0 00003
2 39446 97.8685 100.7423 0050307 39.4444 321.0423 14.96792599 07
| Epoch (UTC): | 24 May 2026 19:40:47 |
| Eccentricity: | 0.0050307 |
| inclination: | 97.8685° |
| perigee height: | 542 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 100.7423° |
| argument of perigee: | 39.4444° |
| revolutions per day: | 14.96792599 |
| mean anomaly at epoch: | 321.0423° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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