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 41745U 16052B 23074.87063178 .00000145 00000-0 00000+0 0 9990
2 41745 1.1046 92.3917 0002685 267.1688 163.9680 1.00033415 6810
| Epoch (UTC): | 15 March 2023 20:53:42 |
| Eccentricity: | 0.0002685 |
| inclination: | 1.1046° |
| perigee height: | 35842 km |
| apogee height: | 35864 km |
| right ascension of ascending node: | 92.3917° |
| argument of perigee: | 267.1688° |
| revolutions per day: | 1.00033415 |
| mean anomaly at epoch: | 163.9680° |
| orbit number at epoch: | 681 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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