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 39974U 87068DA 24352.24606338 .00006426 00000-0 33891-2 0 9993
2 39974 82.5379 166.8886 0020096 235.2667 299.0128 14.13676486540476
| Epoch (UTC): | 17 December 2024 05:54:19 |
| Eccentricity: | 0.0020096 |
| inclination: | 82.5379° |
| perigee height: | 832 km |
| apogee height: | 861 km |
| right ascension of ascending node: | 166.8886° |
| argument of perigee: | 235.2667° |
| revolutions per day: | 14.13676486 |
| mean anomaly at epoch: | 299.0128° |
| orbit number at epoch: | 54047 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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