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 22274.33472726 -.00000010 00000-0 73219-3 0 9999
2 00051 47.2116 281.4075 0105735 128.9401 232.0867 12.18282478765999
| Epoch (UTC): | 01 October 2022 08:02:00 |
| Eccentricity: | 0.0105735 |
| inclination: | 47.2116° |
| perigee height: | 1515 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 281.4075° |
| argument of perigee: | 128.9401° |
| revolutions per day: | 12.18282478 |
| mean anomaly at epoch: | 232.0867° |
| orbit number at epoch: | 76599 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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