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 27601U 02056E 25197.94889140 .00000192 00000-0 81812-4 0 9992
2 27601 98.2809 162.8475 0071158 143.3876 284.8931 14.33525034180319
| Epoch (UTC): | 16 July 2025 22:46:24 |
| Eccentricity: | 0.0071158 |
| inclination: | 98.2809° |
| perigee height: | 729 km |
| apogee height: | 831 km |
| right ascension of ascending node: | 162.8475° |
| argument of perigee: | 143.3876° |
| revolutions per day: | 14.33525034 |
| mean anomaly at epoch: | 284.8931° |
| orbit number at epoch: | 18031 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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