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 27433U 02024D 25197.73186612 .00000227 00000-0 14234-3 0 9993
2 27433 98.9658 241.0030 0014395 17.8384 342.3291 14.14354614193908
| Epoch (UTC): | 16 July 2025 17:33:53 |
| Eccentricity: | 0.0014395 |
| inclination: | 98.9658° |
| perigee height: | 834 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 241.0030° |
| argument of perigee: | 17.8384° |
| revolutions per day: | 14.14354614 |
| mean anomaly at epoch: | 342.3291° |
| orbit number at epoch: | 19390 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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