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 39770U 14029E 23090.94628973 .00029829 00000-0 24767-2 0 9992
2 39770 97.9525 216.2006 0010413 212.1020 147.9580 14.98663183480576
| Epoch (UTC): | 31 March 2023 22:42:39 |
| Eccentricity: | 0.0010413 |
| inclination: | 97.9525° |
| perigee height: | 564 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 216.2006° |
| argument of perigee: | 212.1020° |
| revolutions per day: | 14.98663183 |
| mean anomaly at epoch: | 147.9580° |
| orbit number at epoch: | 48057 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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