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 00029U 60002B 24252.91138012 .00004114 00000-0 60768-3 0 9999
2 00029 48.3765 212.3745 0023129 6.3456 353.7746 14.76765575446531
| Epoch (UTC): | 08 September 2024 21:52:23 |
| Eccentricity: | 0.0023129 |
| inclination: | 48.3765° |
| perigee height: | 623 km |
| apogee height: | 656 km |
| right ascension of ascending node: | 212.3745° |
| argument of perigee: | 6.3456° |
| revolutions per day: | 14.76765575 |
| mean anomaly at epoch: | 353.7746° |
| orbit number at epoch: | 44653 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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