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 23147.86469838 -.00000206 00000-0 -77956-4 0 9995
2 17974 71.0094 16.1494 0015473 312.2499 125.1014 14.17359324864232
| Epoch (UTC): | 27 May 2023 20:45:09 |
| Eccentricity: | 0.0015473 |
| inclination: | 71.0094° |
| perigee height: | 823 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 16.1494° |
| argument of perigee: | 312.2499° |
| revolutions per day: | 14.17359324 |
| mean anomaly at epoch: | 125.1014° |
| orbit number at epoch: | 86423 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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