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 37056U 99025EEQ 24279.70465343 .00016240 00000-0 27403-2 0 9993
2 37056 98.9848 267.2005 0279561 5.2360 355.1648 14.46927500591406
| Epoch (UTC): | 05 October 2024 16:54:42 |
| Eccentricity: | 0.0279561 |
| inclination: | 98.9848° |
| perigee height: | 537 km |
| apogee height: | 934 km |
| right ascension of ascending node: | 267.2005° |
| argument of perigee: | 5.2360° |
| revolutions per day: | 14.46927500 |
| mean anomaly at epoch: | 355.1648° |
| orbit number at epoch: | 59140 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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