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 05104U 71024A 25133.77282921 .00000038 00000-0 13843-3 0 9999
2 05104 88.1732 20.0141 0044608 27.6858 37.7494 12.67877970504138
| Epoch (UTC): | 13 May 2025 18:32:52 |
| Eccentricity: | 0.0044608 |
| inclination: | 88.1732° |
| perigee height: | 1356 km |
| apogee height: | 1425 km |
| right ascension of ascending node: | 20.0141° |
| argument of perigee: | 27.6858° |
| revolutions per day: | 12.67877970 |
| mean anomaly at epoch: | 37.7494° |
| orbit number at epoch: | 50413 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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