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 28538U 05004B 25193.93292869 -.00000066 00000-0 32665-4 0 9992
2 28538 63.8245 63.8469 0215868 274.3243 83.3149 13.43338734 59592
| Epoch (UTC): | 12 July 2025 22:23:25 |
| Eccentricity: | 0.0215868 |
| inclination: | 63.8245° |
| perigee height: | 935 km |
| apogee height: | 1258 km |
| right ascension of ascending node: | 63.8469° |
| argument of perigee: | 274.3243° |
| revolutions per day: | 13.43338734 |
| mean anomaly at epoch: | 83.3149° |
| orbit number at epoch: | 5959 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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