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 23150.88634654 -.00000134 00000-0 -42318-4 0 9995
2 17974 71.0090 9.7817 0015548 308.1165 62.5555 14.17358779864666
| Epoch (UTC): | 30 May 2023 21:16:20 |
| Eccentricity: | 0.0015548 |
| inclination: | 71.0090° |
| perigee height: | 823 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 9.7817° |
| argument of perigee: | 308.1165° |
| revolutions per day: | 14.17358779 |
| mean anomaly at epoch: | 62.5555° |
| orbit number at epoch: | 86466 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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