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 23156.14255894 .00001208 00000-0 21762-3 0 9996
2 27939 98.2418 303.0141 0012801 169.1895 299.1727 14.68362184 52778
| Epoch (UTC): | 05 June 2023 03:25:17 |
| Eccentricity: | 0.0012801 |
| inclination: | 98.2418° |
| perigee height: | 657 km |
| apogee height: | 675 km |
| right ascension of ascending node: | 303.0141° |
| argument of perigee: | 169.1895° |
| revolutions per day: | 14.68362184 |
| mean anomaly at epoch: | 299.1727° |
| orbit number at epoch: | 5277 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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