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 25397U 98043D 24357.87942173 .00000271 00000-0 13740-3 0 9990
2 25397 98.9493 327.6897 0001351 21.9443 338.1792 14.24216305374279
| Epoch (UTC): | 22 December 2024 21:06:22 |
| Eccentricity: | 0.0001351 |
| inclination: | 98.9493° |
| perigee height: | 810 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 327.6897° |
| argument of perigee: | 21.9443° |
| revolutions per day: | 14.24216305 |
| mean anomaly at epoch: | 338.1792° |
| orbit number at epoch: | 37427 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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