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 38770U 12048N 25188.62079065 .00021120 00000-0 40569-3 0 9992
2 38770 64.6409 357.0627 0091435 269.7983 89.2676 15.43458948 65114
| Epoch (UTC): | 07 July 2025 14:53:56 |
| Eccentricity: | 0.0091435 |
| inclination: | 64.6409° |
| perigee height: | 373 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 357.0627° |
| argument of perigee: | 269.7983° |
| revolutions per day: | 15.43458948 |
| mean anomaly at epoch: | 89.2676° |
| orbit number at epoch: | 6511 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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