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 23270.84933358 .00036829 00000-0 24337-2 0 9998
2 39770 97.9966 41.5547 0005914 320.2048 39.8744 15.07279509507594
| Epoch (UTC): | 27 September 2023 20:23:02 |
| Eccentricity: | 0.0005914 |
| inclination: | 97.9966° |
| perigee height: | 540 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 41.5547° |
| argument of perigee: | 320.2048° |
| revolutions per day: | 15.07279509 |
| mean anomaly at epoch: | 39.8744° |
| orbit number at epoch: | 50759 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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