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 23340.48352208 .00000118 00000-0 51333-4 0 9996
2 58 28.3249 146.5245 0164801 119.3707 242.3403 13.46363275110020
| Epoch (UTC): | 06 December 2023 11:36:16 |
| Eccentricity: | 0.0164801 |
| inclination: | 28.3249° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 146.5245° |
| argument of perigee: | 119.3707° |
| revolutions per day: | 13.46363275 |
| mean anomaly at epoch: | 242.3403° |
| orbit number at epoch: | 11002 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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