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 10617U 76067AR 24357.54172784 .00000005 00000-0 18903-3 0 9999
2 10617 65.6340 50.2401 0745489 318.4175 145.7682 12.36355133186964
| Epoch (UTC): | 22 December 2024 13:00:05 |
| Eccentricity: | 0.0745489 |
| inclination: | 65.6340° |
| perigee height: | 933 km |
| apogee height: | 2111 km |
| right ascension of ascending node: | 50.2401° |
| argument of perigee: | 318.4175° |
| revolutions per day: | 12.36355133 |
| mean anomaly at epoch: | 145.7682° |
| orbit number at epoch: | 18696 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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