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 00058U 60013A 23344.56146966 .00000096 00000-0 15519-4 0 9992
2 00058 28.3260 125.8335 0164774 153.1289 207.7898 13.46363415110033
| Epoch (UTC): | 10 December 2023 13:28:30 |
| Eccentricity: | 0.0164774 |
| inclination: | 28.3260° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 125.8335° |
| argument of perigee: | 153.1289° |
| revolutions per day: | 13.46363415 |
| mean anomaly at epoch: | 207.7898° |
| orbit number at epoch: | 11003 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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