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 56503C 23065A 24280.12826389 -.00011917 00000+0 -87916-3 0 2807
2 56503 43.0013 153.8754 0001341 260.6785 142.2033 15.02553239 19
| Epoch (UTC): | 06 October 2024 03:04:42 |
| Eccentricity: | 0.0001341 |
| inclination: | 43.0013° |
| perigee height: | 558 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 153.8754° |
| argument of perigee: | 260.6785° |
| revolutions per day: | 15.02553239 |
| mean anomaly at epoch: | 142.2033° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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