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 39206U 13036A 24260.76909009 .00000059 00000-0 00000-0 0 9991
2 39206 3.7808 41.7022 0055534 177.6256 236.7150 1.00270353 40795
| Epoch (UTC): | 16 September 2024 18:27:29 |
| Eccentricity: | 0.0055534 |
| inclination: | 3.7808° |
| perigee height: | 35552 km |
| apogee height: | 36021 km |
| right ascension of ascending node: | 41.7022° |
| argument of perigee: | 177.6256° |
| revolutions per day: | 1.00270353 |
| mean anomaly at epoch: | 236.7150° |
| orbit number at epoch: | 4079 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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