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 00016U 58002A 22274.29585962 -.00000041 00000-0 -59113-4 0 9995
2 00016 34.2616 261.0243 2027074 162.2823 206.0405 10.48816641546590
| Epoch (UTC): | 01 October 2022 07:06:02 |
| Eccentricity: | 0.2027074 |
| inclination: | 34.2616° |
| perigee height: | 651 km |
| apogee height: | 4225 km |
| right ascension of ascending node: | 261.0243° |
| argument of perigee: | 162.2823° |
| revolutions per day: | 10.48816641 |
| mean anomaly at epoch: | 206.0405° |
| orbit number at epoch: | 54659 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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