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 23331.27684556 -.00000007 00000-0 75241-3 0 9996
2 00051 47.2149 55.9682 0107336 301.5739 57.4607 12.18310904817439
| Epoch (UTC): | 27 November 2023 06:38:39 |
| Eccentricity: | 0.0107336 |
| inclination: | 47.2149° |
| perigee height: | 1514 km |
| apogee height: | 1685 km |
| right ascension of ascending node: | 55.9682° |
| argument of perigee: | 301.5739° |
| revolutions per day: | 12.18310904 |
| mean anomaly at epoch: | 57.4607° |
| orbit number at epoch: | 81743 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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