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 23091.10833955 .00002548 00000-0 45152-3 0 9997
2 27939 98.2290 237.5559 0012887 25.0577 335.1244 14.68132037 43239
| Epoch (UTC): | 01 April 2023 02:36:00 |
| Eccentricity: | 0.0012887 |
| inclination: | 98.2290° |
| perigee height: | 658 km |
| apogee height: | 676 km |
| right ascension of ascending node: | 237.5559° |
| argument of perigee: | 25.0577° |
| revolutions per day: | 14.68132037 |
| mean anomaly at epoch: | 335.1244° |
| orbit number at epoch: | 4323 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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