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 23037.86569564 .00000098 00000-0 13874-3 0 9999
2 00016 34.2642 249.6877 2026633 344.4210 10.1949 10.48810242560097
| Epoch (UTC): | 06 February 2023 20:46:36 |
| Eccentricity: | 0.2026633 |
| inclination: | 34.2642° |
| perigee height: | 651 km |
| apogee height: | 4224 km |
| right ascension of ascending node: | 249.6877° |
| argument of perigee: | 344.4210° |
| revolutions per day: | 10.48810242 |
| mean anomaly at epoch: | 10.1949° |
| orbit number at epoch: | 56009 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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