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 43446U 26142.94842784 +.00000000 +00000-0 +00000-0 0 00005
2 43446 7.0560 67.2228 0010643 166.5711 1.2727 1.02119637 08
| Epoch (UTC): | 22 May 2026 22:45:44 |
| Eccentricity: | 0.0010643 |
| inclination: | 7.0560° |
| perigee height: | 35232 km |
| apogee height: | 35321 km |
| right ascension of ascending node: | 67.2228° |
| argument of perigee: | 166.5711° |
| revolutions per day: | 1.02119637 |
| mean anomaly at epoch: | 1.2727° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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