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 04256U 69082B 21125.41136734 .00000009 00000-0 43563-4 0 9996
2 04256 70.0123 16.4189 0019826 343.8478 16.1994 13.98390715629153
| Epoch (UTC): | 05 May 2021 09:52:22 |
| Eccentricity: | 0.0019826 |
| inclination: | 70.0123° |
| perigee height: | 885 km |
| apogee height: | 914 km |
| right ascension of ascending node: | 16.4189° |
| argument of perigee: | 343.8478° |
| revolutions per day: | 13.98390715 |
| mean anomaly at epoch: | 16.1994° |
| orbit number at epoch: | 62915 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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