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 22148.48259375 -.00000001 00000-0 56810-5 0 9999
2 00016 34.2656 264.4169 2025758 351.6428 5.4715 10.48823367533381
| Epoch (UTC): | 28 May 2022 11:34:56 |
| Eccentricity: | 0.2025758 |
| inclination: | 34.2656° |
| perigee height: | 652 km |
| apogee height: | 4223 km |
| right ascension of ascending node: | 264.4169° |
| argument of perigee: | 351.6428° |
| revolutions per day: | 10.48823367 |
| mean anomaly at epoch: | 5.4715° |
| orbit number at epoch: | 53338 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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