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 22278.37625617 .00012991 00000-0 24621-2 0 9991
2 00085 38.7681 39.4779 0370660 358.7084 1.2686 14.28185689 50790
| Epoch (UTC): | 05 October 2022 09:01:48 |
| Eccentricity: | 0.0370660 |
| inclination: | 38.7681° |
| perigee height: | 532 km |
| apogee height: | 1064 km |
| right ascension of ascending node: | 39.4779° |
| argument of perigee: | 358.7084° |
| revolutions per day: | 14.28185689 |
| mean anomaly at epoch: | 1.2686° |
| orbit number at epoch: | 5079 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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