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 27937U 03041A 22262.94247685 0.00000000 00000-0 00000-0 0 08
2 27937 12.7487 46.2015 0040448 219.0091 140.5682 1.00270000 05
| Epoch (UTC): | 19 September 2022 22:37:10 |
| Eccentricity: | 0.0040448 |
| inclination: | 12.7487° |
| perigee height: | 35616 km |
| apogee height: | 35957 km |
| right ascension of ascending node: | 46.2015° |
| argument of perigee: | 219.0091° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 140.5682° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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