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 25167.84373616 .00000051 00000-0 46542-4 0 9990
2 00005 34.2625 1.9537 1841930 291.2449 50.1669 10.85927253403568
| Epoch (UTC): | 16 June 2025 20:14:58 |
| Eccentricity: | 0.1841930 |
| inclination: | 34.2625° |
| perigee height: | 649 km |
| apogee height: | 3822 km |
| right ascension of ascending node: | 1.9537° |
| argument of perigee: | 291.2449° |
| revolutions per day: | 10.85927253 |
| mean anomaly at epoch: | 50.1669° |
| orbit number at epoch: | 40356 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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