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 10121U 77059B 25191.57671292 .00000108 00000-0 45092-4 0 9993
2 10121 74.0463 126.7606 0017379 112.7348 247.5644 14.37183945512412
| Epoch (UTC): | 10 July 2025 13:50:27 |
| Eccentricity: | 0.0017379 |
| inclination: | 74.0463° |
| perigee height: | 755 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 126.7606° |
| argument of perigee: | 112.7348° |
| revolutions per day: | 14.37183945 |
| mean anomaly at epoch: | 247.5644° |
| orbit number at epoch: | 51241 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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