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 22279.66643534 -.00000063 00000-0 21833-3 0 9990
2 00051 47.2114 264.9110 0105675 144.7404 216.0432 12.18282949766641
| Epoch (UTC): | 06 October 2022 15:59:40 |
| Eccentricity: | 0.0105675 |
| inclination: | 47.2114° |
| perigee height: | 1516 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 264.9110° |
| argument of perigee: | 144.7404° |
| revolutions per day: | 12.18282949 |
| mean anomaly at epoch: | 216.0432° |
| orbit number at epoch: | 76664 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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