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 40042U 14033AJ 24357.94883726 .00022908 00000-0 13731-2 0 9997
2 40042 98.0915 331.3198 0009410 208.0402 152.0321 15.10947353571254
| Epoch (UTC): | 22 December 2024 22:46:19 |
| Eccentricity: | 0.0009410 |
| inclination: | 98.0915° |
| perigee height: | 527 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 331.3198° |
| argument of perigee: | 208.0402° |
| revolutions per day: | 15.10947353 |
| mean anomaly at epoch: | 152.0321° |
| orbit number at epoch: | 57125 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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