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 24263.40484799 .00007732 00000-0 76900-3 0 9996
2 39417 97.7428 217.4013 0047870 206.0283 153.8528 14.91076379585612
| Epoch (UTC): | 19 September 2024 09:42:58 |
| Eccentricity: | 0.0047870 |
| inclination: | 97.7428° |
| perigee height: | 561 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 217.4013° |
| argument of perigee: | 206.0283° |
| revolutions per day: | 14.91076379 |
| mean anomaly at epoch: | 153.8528° |
| orbit number at epoch: | 58561 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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