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 5918U 72022B 22148.15939442 .00000105 00000-0 56076-4 0 9994
2 5918 81.2392 18.7863 0057797 292.8407 66.6664 14.05913606571743
| Epoch (UTC): | 28 May 2022 03:49:31 |
| Eccentricity: | 0.0057797 |
| inclination: | 81.2392° |
| perigee height: | 831 km |
| apogee height: | 915 km |
| right ascension of ascending node: | 18.7863° |
| argument of perigee: | 292.8407° |
| revolutions per day: | 14.05913606 |
| mean anomaly at epoch: | 66.6664° |
| orbit number at epoch: | 57174 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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