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 23088.80463731 .00000313 00000-0 17014-3 0 9999
2 27640 98.7179 98.1816 0014133 1.6398 171.4798 14.19232997 47425
| Epoch (UTC): | 29 March 2023 19:18:40 |
| Eccentricity: | 0.0014133 |
| inclination: | 98.7179° |
| perigee height: | 818 km |
| apogee height: | 838 km |
| right ascension of ascending node: | 98.1816° |
| argument of perigee: | 1.6398° |
| revolutions per day: | 14.19232997 |
| mean anomaly at epoch: | 171.4798° |
| orbit number at epoch: | 4742 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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