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 25407U 98045B 25198.71440840 .00000262 00000-0 15667-3 0 9995
2 25407 71.0128 315.7043 0006933 7.2285 352.8937 14.16146041393838
| Epoch (UTC): | 17 July 2025 17:08:44 |
| Eccentricity: | 0.0006933 |
| inclination: | 71.0128° |
| perigee height: | 833 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 315.7043° |
| argument of perigee: | 7.2285° |
| revolutions per day: | 14.16146041 |
| mean anomaly at epoch: | 352.8937° |
| orbit number at epoch: | 39383 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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