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 22221.37169886 .00003685 00000-0 71599-3 0 9997
2 00085 38.7694 333.6396 0373091 335.1803 23.1402 14.27643847 42645
| Epoch (UTC): | 09 August 2022 08:55:14 |
| Eccentricity: | 0.0373091 |
| inclination: | 38.7694° |
| perigee height: | 532 km |
| apogee height: | 1067 km |
| right ascension of ascending node: | 333.6396° |
| argument of perigee: | 335.1803° |
| revolutions per day: | 14.27643847 |
| mean anomaly at epoch: | 23.1402° |
| orbit number at epoch: | 4264 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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