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 15483U 85006B 25191.57684910 .00000144 00000-0 56700-4 0 9999
2 15483 74.0468 346.5764 0019026 319.1324 110.0960 14.37607456119234
| Epoch (UTC): | 10 July 2025 13:50:39 |
| Eccentricity: | 0.0019026 |
| inclination: | 74.0468° |
| perigee height: | 753 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 346.5764° |
| argument of perigee: | 319.1324° |
| revolutions per day: | 14.37607456 |
| mean anomaly at epoch: | 110.0960° |
| orbit number at epoch: | 11923 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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