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 22176.47607192 -.00000125 00000-0 -39155-3 0 9991
2 00051 47.2106 224.1615 0108772 198.1101 161.5797 12.18283271754068
| Epoch (UTC): | 25 June 2022 11:25:32 |
| Eccentricity: | 0.0108772 |
| inclination: | 47.2106° |
| perigee height: | 1513 km |
| apogee height: | 1687 km |
| right ascension of ascending node: | 224.1615° |
| argument of perigee: | 198.1101° |
| revolutions per day: | 12.18283271 |
| mean anomaly at epoch: | 161.5797° |
| orbit number at epoch: | 75406 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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