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 26740U 94029AEH 24357.45450207 .00114272 00000-0 22514-2 0 9994
2 26740 81.8549 151.5568 0042783 301.9286 57.7803 15.45782006413455
| Epoch (UTC): | 22 December 2024 10:54:28 |
| Eccentricity: | 0.0042783 |
| inclination: | 81.8549° |
| perigee height: | 400 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 151.5568° |
| argument of perigee: | 301.9286° |
| revolutions per day: | 15.45782006 |
| mean anomaly at epoch: | 57.7803° |
| orbit number at epoch: | 41345 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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