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 12715U 81053BK 24357.89688556 .00005662 00000-0 21090-2 0 9992
2 12715 83.1082 168.5074 0063400 96.7980 21.1013 14.30760731237959
| Epoch (UTC): | 22 December 2024 21:31:30 |
| Eccentricity: | 0.0063400 |
| inclination: | 83.1082° |
| perigee height: | 744 km |
| apogee height: | 834 km |
| right ascension of ascending node: | 168.5074° |
| argument of perigee: | 96.7980° |
| revolutions per day: | 14.30760731 |
| mean anomaly at epoch: | 21.1013° |
| orbit number at epoch: | 23795 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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