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 25197.66958647 -.00000076 00000-0 -14728-4 0 9990
2 23705 71.0224 315.7598 0010777 125.2753 234.9380 14.15450361534450
| Epoch (UTC): | 16 July 2025 16:04:12 |
| Eccentricity: | 0.0010777 |
| inclination: | 71.0224° |
| perigee height: | 833 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 315.7598° |
| argument of perigee: | 125.2753° |
| revolutions per day: | 14.15450361 |
| mean anomaly at epoch: | 234.9380° |
| orbit number at epoch: | 53445 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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