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 38342U 12026A 24261.14391800 -.00000182 00000-0 00000+0 0 9993
2 38342 0.0176 252.6622 0002730 293.1723 131.4464 1.00270359 45201
| Epoch (UTC): | 17 September 2024 03:27:14 |
| Eccentricity: | 0.0002730 |
| inclination: | 0.0176° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 252.6622° |
| argument of perigee: | 293.1723° |
| revolutions per day: | 1.00270359 |
| mean anomaly at epoch: | 131.4464° |
| orbit number at epoch: | 4520 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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