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 21292.57074763 .00005309 00000-0 11510-2 0 9996
2 00085 38.7642 42.6544 0376816 163.4482 197.8954 14.22354176 726
| Epoch (UTC): | 19 October 2021 13:41:52 |
| Eccentricity: | 0.0376816 |
| inclination: | 38.7642° |
| perigee height: | 546 km |
| apogee height: | 1088 km |
| right ascension of ascending node: | 42.6544° |
| argument of perigee: | 163.4482° |
| revolutions per day: | 14.22354176 |
| mean anomaly at epoch: | 197.8954° |
| orbit number at epoch: | 72 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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