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 23150.24665099 -.00000107 00000-0 -20826-3 0 9994
2 00051 47.2121 256.0612 0108475 125.1915 235.9088 12.18302580795361
| Epoch (UTC): | 30 May 2023 05:55:10 |
| Eccentricity: | 0.0108475 |
| inclination: | 47.2121° |
| perigee height: | 1513 km |
| apogee height: | 1686 km |
| right ascension of ascending node: | 256.0612° |
| argument of perigee: | 125.1915° |
| revolutions per day: | 12.18302580 |
| mean anomaly at epoch: | 235.9088° |
| orbit number at epoch: | 79536 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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