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 25132.95600945 .00000117 00000-0 47828-4 0 9996
2 00058 28.3292 10.5396 0164885 133.7227 227.7100 13.46410516180089
| Epoch (UTC): | 12 May 2025 22:56:39 |
| Eccentricity: | 0.0164885 |
| inclination: | 28.3292° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 10.5396° |
| argument of perigee: | 133.7227° |
| revolutions per day: | 13.46410516 |
| mean anomaly at epoch: | 227.7100° |
| orbit number at epoch: | 18008 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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