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 42279U 95015GV 24280.03274115 .00077700 00000-0 20338-1 0 9991
2 42279 98.7410 312.3744 0014055 153.1349 207.0573 14.48760983491503
| Epoch (UTC): | 06 October 2024 00:47:08 |
| Eccentricity: | 0.0014055 |
| inclination: | 98.7410° |
| perigee height: | 720 km |
| apogee height: | 739 km |
| right ascension of ascending node: | 312.3744° |
| argument of perigee: | 153.1349° |
| revolutions per day: | 14.48760983 |
| mean anomaly at epoch: | 207.0573° |
| orbit number at epoch: | 49150 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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