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 25166.76607422 .00000095 00000-0 18712-4 0 9994
2 00058 28.3249 198.9913 0164927 53.6670 307.8979 13.46412452184647
| Epoch (UTC): | 15 June 2025 18:23:08 |
| Eccentricity: | 0.0164927 |
| inclination: | 28.3249° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 198.9913° |
| argument of perigee: | 53.6670° |
| revolutions per day: | 13.46412452 |
| mean anomaly at epoch: | 307.8979° |
| orbit number at epoch: | 18464 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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