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 00011U 59001A 25348.30828400 .00000451 00000-0 24117-3 0 9992
2 00011 32.8673 64.6861 1447561 84.9934 291.3759 11.90150840513430
| Epoch (UTC): | 14 December 2025 07:23:55 |
| Eccentricity: | 0.1447561 |
| inclination: | 32.8673° |
| perigee height: | 552 km |
| apogee height: | 2898 km |
| right ascension of ascending node: | 64.6861° |
| argument of perigee: | 84.9934° |
| revolutions per day: | 11.90150840 |
| mean anomaly at epoch: | 291.3759° |
| orbit number at epoch: | 51343 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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