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 06257U 72085B 24255.78088464 .00000209 00000-0 11742-3 0 9994
2 06257 81.2585 125.4334 0055160 248.6643 110.8633 14.06706822660834
| Epoch (UTC): | 11 September 2024 18:44:28 |
| Eccentricity: | 0.0055160 |
| inclination: | 81.2585° |
| perigee height: | 830 km |
| apogee height: | 910 km |
| right ascension of ascending node: | 125.4334° |
| argument of perigee: | 248.6643° |
| revolutions per day: | 14.06706822 |
| mean anomaly at epoch: | 110.8633° |
| orbit number at epoch: | 66083 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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