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 27946U 03043B 22230.21298834 -.00000142 00000-0 33530-3 0 9999
2 27946 7.4919 125.0781 7177936 167.0571 232.4244 2.23498673154310
| Epoch (UTC): | 18 August 2022 05:06:42 |
| Eccentricity: | 0.7177936 |
| inclination: | 7.4919° |
| perigee height: | 595 km |
| apogee height: | 36069 km |
| right ascension of ascending node: | 125.0781° |
| argument of perigee: | 167.0571° |
| revolutions per day: | 2.23498673 |
| mean anomaly at epoch: | 232.4244° |
| orbit number at epoch: | 15431 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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