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 11327U 79030B 25162.85003442 .00000086 00000-0 72083-4 0 9993
2 11327 82.9501 290.1816 0026291 295.5331 183.7474 13.77179697320316
| Epoch (UTC): | 11 June 2025 20:24:02 |
| Eccentricity: | 0.0026291 |
| inclination: | 82.9501° |
| perigee height: | 954 km |
| apogee height: | 993 km |
| right ascension of ascending node: | 290.1816° |
| argument of perigee: | 295.5331° |
| revolutions per day: | 13.77179697 |
| mean anomaly at epoch: | 183.7474° |
| orbit number at epoch: | 32031 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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