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 25197.92858805 .00000306 00000-0 29758-3 0 9993
2 00082 38.8524 164.9085 1166959 43.2648 325.3966 12.27671264 35593
| Epoch (UTC): | 16 July 2025 22:17:10 |
| Eccentricity: | 0.1166959 |
| inclination: | 38.8524° |
| perigee height: | 633 km |
| apogee height: | 2485 km |
| right ascension of ascending node: | 164.9085° |
| argument of perigee: | 43.2648° |
| revolutions per day: | 12.27671264 |
| mean anomaly at epoch: | 325.3966° |
| orbit number at epoch: | 3559 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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