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 23275.58196528 -.00000013 00000-0 69848-3 0 9997
2 00051 47.2112 228.2845 0105682 136.9677 223.9434 12.18304142810649
| Epoch (UTC): | 02 October 2023 13:58:01 |
| Eccentricity: | 0.0105682 |
| inclination: | 47.2112° |
| perigee height: | 1515 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 228.2845° |
| argument of perigee: | 136.9677° |
| revolutions per day: | 12.18304142 |
| mean anomaly at epoch: | 223.9434° |
| orbit number at epoch: | 81064 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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