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 25198.46002136 .00026823 00000-0 41454-3 0 9994
2 18748 82.4548 354.1576 0005502 44.9176 315.2521 15.53930449 54310
| Epoch (UTC): | 17 July 2025 11:02:25 |
| Eccentricity: | 0.0005502 |
| inclination: | 82.4548° |
| perigee height: | 401 km |
| apogee height: | 409 km |
| right ascension of ascending node: | 354.1576° |
| argument of perigee: | 44.9176° |
| revolutions per day: | 15.53930449 |
| mean anomaly at epoch: | 315.2521° |
| orbit number at epoch: | 5431 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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