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 00005U 58002B 22018.87466262 .00000162 00000-0 23387-3 0 9999
2 00005 34.2408 240.2621 1843357 84.3192 296.3552 10.84848467268292
| Epoch (UTC): | 18 January 2022 20:59:30 |
| Eccentricity: | 0.1843357 |
| inclination: | 34.2408° |
| perigee height: | 652 km |
| apogee height: | 3830 km |
| right ascension of ascending node: | 240.2621° |
| argument of perigee: | 84.3192° |
| revolutions per day: | 10.84848467 |
| mean anomaly at epoch: | 296.3552° |
| orbit number at epoch: | 26829 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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