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 18748U 88001A 25188.54177020 .00022063 00000-0 34621-3 0 9997
2 18748 82.4535 4.5982 0006255 77.3469 282.8483 15.53509237 52528
| Epoch (UTC): | 07 July 2025 13:00:08 |
| Eccentricity: | 0.0006255 |
| inclination: | 82.4535° |
| perigee height: | 402 km |
| apogee height: | 411 km |
| right ascension of ascending node: | 4.5982° |
| argument of perigee: | 77.3469° |
| revolutions per day: | 15.53509237 |
| mean anomaly at epoch: | 282.8483° |
| orbit number at epoch: | 5252 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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