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 44408U 19038Y 24357.97614298 .00023262 00000-0 67365-3 0 9993
2 44408 97.7233 355.5946 0014986 164.9140 195.2552 15.35475917302767
| Epoch (UTC): | 22 December 2024 23:25:38 |
| Eccentricity: | 0.0014986 |
| inclination: | 97.7233° |
| perigee height: | 449 km |
| apogee height: | 470 km |
| right ascension of ascending node: | 355.5946° |
| argument of perigee: | 164.9140° |
| revolutions per day: | 15.35475917 |
| mean anomaly at epoch: | 195.2552° |
| orbit number at epoch: | 30276 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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