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 10974U 78067B 23027.47643125 .00000788 00000-0 83505-4 0 9993
2 10974 82.4812 26.9851 0018088 32.5336 327.6991 14.87746494391190
| Epoch (UTC): | 27 January 2023 11:26:03 |
| Eccentricity: | 0.0018088 |
| inclination: | 82.4812° |
| perigee height: | 592 km |
| apogee height: | 617 km |
| right ascension of ascending node: | 26.9851° |
| argument of perigee: | 32.5336° |
| revolutions per day: | 14.87746494 |
| mean anomaly at epoch: | 327.6991° |
| orbit number at epoch: | 39119 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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