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 36340U 82025AA 24352.88590291 .00015885 00000-0 49132-2 0 9999
2 36340 82.5203 187.6637 0024123 283.3861 76.4642 14.41006622121570
| Epoch (UTC): | 17 December 2024 21:15:42 |
| Eccentricity: | 0.0024123 |
| inclination: | 82.5203° |
| perigee height: | 738 km |
| apogee height: | 772 km |
| right ascension of ascending node: | 187.6637° |
| argument of perigee: | 283.3861° |
| revolutions per day: | 14.41006622 |
| mean anomaly at epoch: | 76.4642° |
| orbit number at epoch: | 12157 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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