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 40074U 14037F 24281.09560053 .00030213 00000-0 26124-2 0 9991
2 40074 98.3456 218.1453 0006323 73.8586 286.3329 14.97114907555503
| Epoch (UTC): | 07 October 2024 02:17:39 |
| Eccentricity: | 0.0006323 |
| inclination: | 98.3456° |
| perigee height: | 571 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 218.1453° |
| argument of perigee: | 73.8586° |
| revolutions per day: | 14.97114907 |
| mean anomaly at epoch: | 286.3329° |
| orbit number at epoch: | 55550 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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