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 25262U 98018A 25200.18488857 .00031780 00000-0 66320-3 0 9990
2 25262 86.3809 39.9633 0085326 126.1820 234.7367 15.41457513452177
| Epoch (UTC): | 19 July 2025 04:26:14 |
| Eccentricity: | 0.0085326 |
| inclination: | 86.3809° |
| perigee height: | 383 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 39.9633° |
| argument of perigee: | 126.1820° |
| revolutions per day: | 15.41457513 |
| mean anomaly at epoch: | 234.7367° |
| orbit number at epoch: | 45217 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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