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 39224U 13035E 23337.51131239 .00003060 00000-0 10662-2 0 9991
2 39224 97.8805 177.2811 0167990 73.5878 288.3697 14.28351961534810
| Epoch (UTC): | 03 December 2023 12:16:17 |
| Eccentricity: | 0.0167990 |
| inclination: | 97.8805° |
| perigee height: | 677 km |
| apogee height: | 918 km |
| right ascension of ascending node: | 177.2811° |
| argument of perigee: | 73.5878° |
| revolutions per day: | 14.28351961 |
| mean anomaly at epoch: | 288.3697° |
| orbit number at epoch: | 53481 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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