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 23705U 95058B 25196.75087530 -.00000122 00000-0 -38143-4 0 9992
2 23705 71.0224 317.6885 0010784 126.9133 233.2979 14.15450452534321
| Epoch (UTC): | 15 July 2025 18:01:15 |
| Eccentricity: | 0.0010784 |
| inclination: | 71.0224° |
| perigee height: | 833 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 317.6885° |
| argument of perigee: | 126.9133° |
| revolutions per day: | 14.15450452 |
| mean anomaly at epoch: | 233.2979° |
| orbit number at epoch: | 53432 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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