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 23152.04330694 -.00000060 00000-0 -57332-5 0 9993
2 17974 71.0089 7.3435 0015574 306.5807 205.7028 14.17358753864824
| Epoch (UTC): | 01 June 2023 01:02:21 |
| Eccentricity: | 0.0015574 |
| inclination: | 71.0089° |
| perigee height: | 823 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 7.3435° |
| argument of perigee: | 306.5807° |
| revolutions per day: | 14.17358753 |
| mean anomaly at epoch: | 205.7028° |
| orbit number at epoch: | 86482 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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