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 23657U 95046A 25193.73481939 .00001093 00000-0 10209-3 0 9999
2 23657 82.5242 5.0905 0019825 25.9178 334.3030 14.93115776615309
| Epoch (UTC): | 12 July 2025 17:38:08 |
| Eccentricity: | 0.0019825 |
| inclination: | 82.5242° |
| perigee height: | 574 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 5.0905° |
| argument of perigee: | 25.9178° |
| revolutions per day: | 14.93115776 |
| mean anomaly at epoch: | 334.3030° |
| orbit number at epoch: | 61530 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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