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 17974U 87041B 23154.56728083 .00000109 00000-0 77682-4 0 9996
2 17974 71.0085 2.0241 0015614 303.1912 123.7874 14.17359091864949
| Epoch (UTC): | 03 June 2023 13:36:53 |
| Eccentricity: | 0.0015614 |
| inclination: | 71.0085° |
| perigee height: | 823 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 2.0241° |
| argument of perigee: | 303.1912° |
| revolutions per day: | 14.17359091 |
| mean anomaly at epoch: | 123.7874° |
| orbit number at epoch: | 86494 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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