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 22220.44252553 -.00000053 00000-0 30196-3 0 9990
2 00051 47.2130 88.1375 0107754 328.7623 30.6794 12.18283351759422
| Epoch (UTC): | 08 August 2022 10:37:14 |
| Eccentricity: | 0.0107754 |
| inclination: | 47.2130° |
| perigee height: | 1514 km |
| apogee height: | 1686 km |
| right ascension of ascending node: | 88.1375° |
| argument of perigee: | 328.7623° |
| revolutions per day: | 12.18283351 |
| mean anomaly at epoch: | 30.6794° |
| orbit number at epoch: | 75942 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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