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 37839U 11058B 24357.35040303 .00000706 00000-0 22982-3 0 9993
2 37839 19.9628 359.5791 0018547 212.8037 277.6046 14.13457028682265
| Epoch (UTC): | 22 December 2024 08:24:34 |
| Eccentricity: | 0.0018547 |
| inclination: | 19.9628° |
| perigee height: | 834 km |
| apogee height: | 861 km |
| right ascension of ascending node: | 359.5791° |
| argument of perigee: | 212.8037° |
| revolutions per day: | 14.13457028 |
| mean anomaly at epoch: | 277.6046° |
| orbit number at epoch: | 68226 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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