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 39150U 13018A 24358.20553126 .00001859 00000-0 27378-3 0 9990
2 39150 97.9711 68.3580 0018176 208.1329 151.8900 14.76473726628458
| Epoch (UTC): | 23 December 2024 04:55:57 |
| Eccentricity: | 0.0018176 |
| inclination: | 97.9711° |
| perigee height: | 628 km |
| apogee height: | 653 km |
| right ascension of ascending node: | 68.3580° |
| argument of perigee: | 208.1329° |
| revolutions per day: | 14.76473726 |
| mean anomaly at epoch: | 151.8900° |
| orbit number at epoch: | 62845 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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