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 23029.91434077 -.00000061 00000-0 23497-3 0 9998
2 00051 47.2111 268.3598 0107454 125.5361 235.5503 12.18291896780699
| Epoch (UTC): | 29 January 2023 21:56:39 |
| Eccentricity: | 0.0107454 |
| inclination: | 47.2111° |
| perigee height: | 1514 km |
| apogee height: | 1686 km |
| right ascension of ascending node: | 268.3598° |
| argument of perigee: | 125.5361° |
| revolutions per day: | 12.18291896 |
| mean anomaly at epoch: | 235.5503° |
| orbit number at epoch: | 78069 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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