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 5U 58002B 25173.54799685 -.00000002 00000-0 -10669-4 0 9991
2 5 34.2585 344.3524 1841713 316.9515 30.0574 10.85927156404274
| Epoch (UTC): | 22 June 2025 13:09:06 |
| Eccentricity: | 0.1841713 |
| inclination: | 34.2585° |
| perigee height: | 649 km |
| apogee height: | 3822 km |
| right ascension of ascending node: | 344.3524° |
| argument of perigee: | 316.9515° |
| revolutions per day: | 10.85927156 |
| mean anomaly at epoch: | 30.0574° |
| orbit number at epoch: | 40427 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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