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 25196.91449893 .00021922 00000-0 33981-3 0 9998
2 18748 82.4548 355.7842 0005681 50.1257 310.0495 15.53852544 53827
| Epoch (UTC): | 15 July 2025 21:56:52 |
| Eccentricity: | 0.0005681 |
| inclination: | 82.4548° |
| perigee height: | 401 km |
| apogee height: | 409 km |
| right ascension of ascending node: | 355.7842° |
| argument of perigee: | 50.1257° |
| revolutions per day: | 15.53852544 |
| mean anomaly at epoch: | 310.0495° |
| orbit number at epoch: | 5382 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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