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 27640U 03001A 24282.00400053 .00000718 00000-0 36078-3 0 9996
2 27640 98.7161 287.4395 0013944 185.8220 174.2796 14.19588249126600
| Epoch (UTC): | 08 October 2024 00:05:45 |
| Eccentricity: | 0.0013944 |
| inclination: | 98.7161° |
| perigee height: | 817 km |
| apogee height: | 837 km |
| right ascension of ascending node: | 287.4395° |
| argument of perigee: | 185.8220° |
| revolutions per day: | 14.19588249 |
| mean anomaly at epoch: | 174.2796° |
| orbit number at epoch: | 12660 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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