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 00082U 61004B 25138.77562667 .00000557 00000-0 49773-3 0 9996
2 00082 38.8569 24.5276 1166684 117.0519 255.3979 12.27633271 28322
| Epoch (UTC): | 18 May 2025 18:36:54 |
| Eccentricity: | 0.1166684 |
| inclination: | 38.8569° |
| perigee height: | 633 km |
| apogee height: | 2485 km |
| right ascension of ascending node: | 24.5276° |
| argument of perigee: | 117.0519° |
| revolutions per day: | 12.27633271 |
| mean anomaly at epoch: | 255.3979° |
| orbit number at epoch: | 2832 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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