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 27640U 03001A 23156.87322948 .00000109 00000-0 72778-4 0 9998
2 27640 98.7143 165.1585 0014631 156.4691 203.7157 14.19263769 57118
| Epoch (UTC): | 05 June 2023 20:57:27 |
| Eccentricity: | 0.0014631 |
| inclination: | 98.7143° |
| perigee height: | 817 km |
| apogee height: | 838 km |
| right ascension of ascending node: | 165.1585° |
| argument of perigee: | 156.4691° |
| revolutions per day: | 14.19263769 |
| mean anomaly at epoch: | 203.7157° |
| orbit number at epoch: | 5711 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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