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 27665U 03005C 25188.85576321 .00000099 00000-0 71386-4 0 9992
2 27665 39.5744 241.1039 0009034 321.5212 206.5289 14.29404818171745
| Epoch (UTC): | 07 July 2025 20:32:17 |
| Eccentricity: | 0.0009034 |
| inclination: | 39.5744° |
| perigee height: | 787 km |
| apogee height: | 800 km |
| right ascension of ascending node: | 241.1039° |
| argument of perigee: | 321.5212° |
| revolutions per day: | 14.29404818 |
| mean anomaly at epoch: | 206.5289° |
| orbit number at epoch: | 17174 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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