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 24262.87684020 .00018743 00000-0 63457-3 0 9993
2 44408 97.7208 256.3166 0018188 143.2833 216.9657 15.30485386288191
| Epoch (UTC): | 18 September 2024 21:02:38 |
| Eccentricity: | 0.0018188 |
| inclination: | 97.7208° |
| perigee height: | 462 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 256.3166° |
| argument of perigee: | 143.2833° |
| revolutions per day: | 15.30485386 |
| mean anomaly at epoch: | 216.9657° |
| orbit number at epoch: | 28819 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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