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 00050U 60009B 24250.54572453 -.00000081 00000-0 35543-4 0 9992
2 00050 47.2343 15.0501 0113632 241.4772 117.4537 12.20144362858504
| Epoch (UTC): | 06 September 2024 13:05:50 |
| Eccentricity: | 0.0113632 |
| inclination: | 47.2343° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 15.0501° |
| argument of perigee: | 241.4772° |
| revolutions per day: | 12.20144362 |
| mean anomaly at epoch: | 117.4537° |
| orbit number at epoch: | 85850 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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