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 data is extracted from the following two-line orbital elements,
1 43446U 18036F 25109.25149154 -.00000159 00000-0 00000+0 0 9992
2 43446 6.0793 71.9581 0009989 151.2504 313.6339 1.02122869 22577
| Epoch (UTC): | 19 April 2025 06:02:08 |
| Eccentricity: | 0.0009989 |
| inclination: | 6.0793° |
| perigee height: | 35233 km |
| apogee height: | 35317 km |
| right ascension of ascending node: | 71.9581° |
| argument of perigee: | 151.2504° |
| revolutions per day: | 1.02122869 |
| mean anomaly at epoch: | 313.6339° |
| orbit number at epoch: | 2257 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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