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 23092.26696042 .00002670 00000-0 47253-3 0 9999
2 27939 98.2287 238.7214 0012724 21.7359 338.4379 14.68138780 43402
| Epoch (UTC): | 02 April 2023 06:24:25 |
| Eccentricity: | 0.0012724 |
| inclination: | 98.2287° |
| perigee height: | 658 km |
| apogee height: | 676 km |
| right ascension of ascending node: | 238.7214° |
| argument of perigee: | 21.7359° |
| revolutions per day: | 14.68138780 |
| mean anomaly at epoch: | 338.4379° |
| orbit number at epoch: | 4340 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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