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 23087U 94023A 25199.70816694 -.00000156 00000-0 -57022-4 0 9999
2 23087 71.0539 304.6051 0008114 12.2533 347.8785 14.14302857611720
| Epoch (UTC): | 18 July 2025 16:59:45 |
| Eccentricity: | 0.0008114 |
| inclination: | 71.0539° |
| perigee height: | 839 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 304.6051° |
| argument of perigee: | 12.2533° |
| revolutions per day: | 14.14302857 |
| mean anomaly at epoch: | 347.8785° |
| orbit number at epoch: | 61172 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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