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 00085U 61004C 24357.45464869 .00172412 00000-0 13952-1 0 9999
2 00085 38.7166 50.4331 0170865 223.1025 135.6255 14.87567086168075
| Epoch (UTC): | 22 December 2024 10:54:41 |
| Eccentricity: | 0.0170865 |
| inclination: | 38.7166° |
| perigee height: | 486 km |
| apogee height: | 725 km |
| right ascension of ascending node: | 50.4331° |
| argument of perigee: | 223.1025° |
| revolutions per day: | 14.87567086 |
| mean anomaly at epoch: | 135.6255° |
| orbit number at epoch: | 16807 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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