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 51U 60009C 23038.52702951 -.00000006 00000-0 76900-3 0 9990
2 51 47.2100 241.7118 0107774 151.1816 209.4981 12.18292954781737
| Epoch (UTC): | 07 February 2023 12:38:55 |
| Eccentricity: | 0.0107774 |
| inclination: | 47.2100° |
| perigee height: | 1514 km |
| apogee height: | 1686 km |
| right ascension of ascending node: | 241.7118° |
| argument of perigee: | 151.1816° |
| revolutions per day: | 12.18292954 |
| mean anomaly at epoch: | 209.4981° |
| orbit number at epoch: | 78173 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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