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 00051U 60009C 25341.27270513 -.00000048 00000-0 35787-3 0 9999
2 00051 47.2135 283.2134 0111238 345.6652 14.0991 12.18376643907775
| Epoch (UTC): | 07 December 2025 06:32:41 |
| Eccentricity: | 0.0111238 |
| inclination: | 47.2135° |
| perigee height: | 1511 km |
| apogee height: | 1688 km |
| right ascension of ascending node: | 283.2134° |
| argument of perigee: | 345.6652° |
| revolutions per day: | 12.18376643 |
| mean anomaly at epoch: | 14.0991° |
| orbit number at epoch: | 90777 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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