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 00051U 60009C 23026.96140761 -.00000058 00000-0 26385-3 0 9999
2 00051 47.2119 277.4959 0107281 116.7592 244.4220 12.18291665780335
| Epoch (UTC): | 26 January 2023 23:04:25 |
| Eccentricity: | 0.0107281 |
| inclination: | 47.2119° |
| perigee height: | 1514 km |
| apogee height: | 1685 km |
| right ascension of ascending node: | 277.4959° |
| argument of perigee: | 116.7592° |
| revolutions per day: | 12.18291665 |
| mean anomaly at epoch: | 244.4220° |
| orbit number at epoch: | 78033 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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