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 37854U 11061E 24153.80595276 .16898415 55633-5 16987-3 0 9996
2 37854 101.6462 337.6418 0013235 287.7108 72.2736 16.50358911691178
| Epoch (UTC): | 01 June 2024 19:20:34 |
| Eccentricity: | 0.0013235 |
| inclination: | 101.6462° |
| perigee height: | 130 km |
| apogee height: | 147 km |
| right ascension of ascending node: | 337.6418° |
| argument of perigee: | 287.7108° |
| revolutions per day: | 16.50358911 |
| mean anomaly at epoch: | 72.2736° |
| orbit number at epoch: | 69117 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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