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 39151U 13018B 25196.82583823 .00001932 00000-0 20127-3 0 9994
2 39151 98.0776 326.4985 0013251 185.2426 174.8654 14.90984961660542
| Epoch (UTC): | 15 July 2025 19:49:12 |
| Eccentricity: | 0.0013251 |
| inclination: | 98.0776° |
| perigee height: | 585 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 326.4985° |
| argument of perigee: | 185.2426° |
| revolutions per day: | 14.90984961 |
| mean anomaly at epoch: | 174.8654° |
| orbit number at epoch: | 66054 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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