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 00005U 58002B 25171.79985153 .00000012 00000-0 39710-5 0 9991
2 00005 34.2599 349.7470 1841781 309.0722 35.9649 10.85927235403999
| Epoch (UTC): | 20 June 2025 19:11:47 |
| Eccentricity: | 0.1841781 |
| inclination: | 34.2599° |
| perigee height: | 649 km |
| apogee height: | 3822 km |
| right ascension of ascending node: | 349.7470° |
| argument of perigee: | 309.0722° |
| revolutions per day: | 10.85927235 |
| mean anomaly at epoch: | 35.9649° |
| orbit number at epoch: | 40399 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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