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 24260.85472932 .00009949 00000-0 98900-3 0 9994
2 39417 97.7422 214.8989 0047599 214.7037 145.1074 14.91030094585232
| Epoch (UTC): | 16 September 2024 20:30:48 |
| Eccentricity: | 0.0047599 |
| inclination: | 97.7422° |
| perigee height: | 561 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 214.8989° |
| argument of perigee: | 214.7037° |
| revolutions per day: | 14.91030094 |
| mean anomaly at epoch: | 145.1074° |
| orbit number at epoch: | 58523 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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