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 is defined by the following mean orbital elements,
1 37851U 11061B 24224.58186504 .16214664 55693-5 28808-3 0 9996
2 37851 101.6846 77.6320 0012470 240.2417 119.7630 16.46878935701081
| Epoch (UTC): | 11 August 2024 13:57:53 |
| Eccentricity: | 0.0012470 |
| inclination: | 101.6846° |
| perigee height: | 139 km |
| apogee height: | 156 km |
| right ascension of ascending node: | 77.6320° |
| argument of perigee: | 240.2417° |
| revolutions per day: | 16.46878935 |
| mean anomaly at epoch: | 119.7630° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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