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 34487U 97051GC 24357.93500755 .00001803 00000-0 53667-3 0 9995
2 34487 86.3456 165.0026 0029975 221.2669 292.9035 14.42396929831483
| Epoch (UTC): | 22 December 2024 22:26:24 |
| Eccentricity: | 0.0029975 |
| inclination: | 86.3456° |
| perigee height: | 729 km |
| apogee height: | 772 km |
| right ascension of ascending node: | 165.0026° |
| argument of perigee: | 221.2669° |
| revolutions per day: | 14.42396929 |
| mean anomaly at epoch: | 292.9035° |
| orbit number at epoch: | 83148 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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