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 07493U 74083B 25133.74424506 .00000078 00000-0 38085-4 0 9994
2 07493 81.1600 215.1703 0082283 242.2465 117.0343 14.07942225594719
| Epoch (UTC): | 13 May 2025 17:51:42 |
| Eccentricity: | 0.0082283 |
| inclination: | 81.1600° |
| perigee height: | 807 km |
| apogee height: | 926 km |
| right ascension of ascending node: | 215.1703° |
| argument of perigee: | 242.2465° |
| revolutions per day: | 14.07942225 |
| mean anomaly at epoch: | 117.0343° |
| orbit number at epoch: | 59471 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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