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 25315.56554410 .00000098 00000-0 97450-4 0 9992
2 00005 34.2573 265.9539 1842037 237.2912 103.6735 10.85926272419620
| Epoch (UTC): | 11 November 2025 13:34:23 |
| Eccentricity: | 0.1842037 |
| inclination: | 34.2573° |
| perigee height: | 649 km |
| apogee height: | 3822 km |
| right ascension of ascending node: | 265.9539° |
| argument of perigee: | 237.2912° |
| revolutions per day: | 10.85926272 |
| mean anomaly at epoch: | 103.6735° |
| orbit number at epoch: | 41962 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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