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 58U 60013A 22279.35348674 .00000108 00000-0 31397-4 0 9991
2 58 28.3264 148.4878 0165009 191.2150 168.4687 13.46338954 52553
| Epoch (UTC): | 06 October 2022 08:29:01 |
| Eccentricity: | 0.0165009 |
| inclination: | 28.3264° |
| perigee height: | 962 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 148.4878° |
| argument of perigee: | 191.2150° |
| revolutions per day: | 13.46338954 |
| mean anomaly at epoch: | 168.4687° |
| orbit number at epoch: | 5255 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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