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 23334.03270363 .00000130 00000-0 71872-4 0 9995
2 58 28.3249 179.2568 0164796 65.9373 295.8321 13.46362754109154
| Epoch (UTC): | 30 November 2023 00:47:05 |
| Eccentricity: | 0.0164796 |
| inclination: | 28.3249° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 179.2568° |
| argument of perigee: | 65.9373° |
| revolutions per day: | 13.46362754 |
| mean anomaly at epoch: | 295.8321° |
| orbit number at epoch: | 10915 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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