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 40021U 14033M 23033.37499362 .00008111 00000-0 74398-3 0 9997
2 40021 98.0423 353.4121 0012019 12.8982 347.2543 14.95102885469029
| Epoch (UTC): | 02 February 2023 08:59:59 |
| Eccentricity: | 0.0012019 |
| inclination: | 98.0423° |
| perigee height: | 573 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 353.4121° |
| argument of perigee: | 12.8982° |
| revolutions per day: | 14.95102885 |
| mean anomaly at epoch: | 347.2543° |
| orbit number at epoch: | 46902 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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