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 25166.64777144 .00000049 00000-0 42682-4 0 9999
2 00005 34.2630 5.6437 1841963 285.8562 54.7346 10.85927130403437
| Epoch (UTC): | 15 June 2025 15:32:47 |
| Eccentricity: | 0.1841963 |
| inclination: | 34.2630° |
| perigee height: | 649 km |
| apogee height: | 3822 km |
| right ascension of ascending node: | 5.6437° |
| argument of perigee: | 285.8562° |
| revolutions per day: | 10.85927130 |
| mean anomaly at epoch: | 54.7346° |
| orbit number at epoch: | 40343 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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