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 23331.94510836 .00051782 00000-0 29355-2 0 9999
2 39770 98.0016 105.3320 0004681 132.1951 227.9677 15.12782131516819
| Epoch (UTC): | 27 November 2023 22:40:57 |
| Eccentricity: | 0.0004681 |
| inclination: | 98.0016° |
| perigee height: | 524 km |
| apogee height: | 531 km |
| right ascension of ascending node: | 105.3320° |
| argument of perigee: | 132.1951° |
| revolutions per day: | 15.12782131 |
| mean anomaly at epoch: | 227.9677° |
| orbit number at epoch: | 51681 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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