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 22146.67236365 .00000007 00000-0 12795-4 0 9990
2 00016 34.2672 269.6456 2025783 344.0062 10.4697 10.48823383533195
| Epoch (UTC): | 26 May 2022 16:08:12 |
| Eccentricity: | 0.2025783 |
| inclination: | 34.2672° |
| perigee height: | 652 km |
| apogee height: | 4223 km |
| right ascension of ascending node: | 269.6456° |
| argument of perigee: | 344.0062° |
| revolutions per day: | 10.48823383 |
| mean anomaly at epoch: | 10.4697° |
| orbit number at epoch: | 53319 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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