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 27939U 03042A 23087.83691062 .00002221 00000-0 39489-3 0 9997
2 27939 98.2290 234.2644 0012896 35.2690 324.9366 14.68114940 42757
| Epoch (UTC): | 28 March 2023 20:05:09 |
| Eccentricity: | 0.0012896 |
| inclination: | 98.2290° |
| perigee height: | 658 km |
| apogee height: | 676 km |
| right ascension of ascending node: | 234.2644° |
| argument of perigee: | 35.2690° |
| revolutions per day: | 14.68114940 |
| mean anomaly at epoch: | 324.9366° |
| orbit number at epoch: | 4275 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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