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 47688U 21006EP 22278.12072417 .00028229 00000-0 13891-2 0 9994
2 47688 97.4321 334.8786 0008632 244.0450 115.9895 15.17926817 94837
| Epoch (UTC): | 05 October 2022 02:53:50 |
| Eccentricity: | 0.0008632 |
| inclination: | 97.4321° |
| perigee height: | 506 km |
| apogee height: | 518 km |
| right ascension of ascending node: | 334.8786° |
| argument of perigee: | 244.0450° |
| revolutions per day: | 15.17926817 |
| mean anomaly at epoch: | 115.9895° |
| orbit number at epoch: | 9483 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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