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 25868U 99040C 24220.50271216 .00009837 00000-0 93895-3 0 9999
2 25868 28.4696 14.5609 4425455 333.0142 9.5831 6.63974762567808
| Epoch (UTC): | 07 August 2024 12:03:54 |
| Eccentricity: | 0.4425455 |
| inclination: | 28.4696° |
| perigee height: | 287 km |
| apogee height: | 10871 km |
| right ascension of ascending node: | 14.5609° |
| argument of perigee: | 333.0142° |
| revolutions per day: | 6.63974762 |
| mean anomaly at epoch: | 9.5831° |
| orbit number at epoch: | 56780 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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