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 39417U 13066B 25108.82928454 .00007865 00000-0 69233-3 0 9990
2 39417 97.7763 66.1542 0042977 222.8402 136.9468 14.96050736617178
| Epoch (UTC): | 18 April 2025 19:54:10 |
| Eccentricity: | 0.0042977 |
| inclination: | 97.7763° |
| perigee height: | 549 km |
| apogee height: | 609 km |
| right ascension of ascending node: | 66.1542° |
| argument of perigee: | 222.8402° |
| revolutions per day: | 14.96050736 |
| mean anomaly at epoch: | 136.9468° |
| orbit number at epoch: | 61717 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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