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 40074U 14037F 22182.90159971 .00001095 00000-0 13399-3 0 9999
2 40074 98.3812 64.3272 0002991 241.6407 118.4500 14.85443969432211
| Epoch (UTC): | 01 July 2022 21:38:18 |
| Eccentricity: | 0.0002991 |
| inclination: | 98.3812° |
| perigee height: | 610 km |
| apogee height: | 614 km |
| right ascension of ascending node: | 64.3272° |
| argument of perigee: | 241.6407° |
| revolutions per day: | 14.85443969 |
| mean anomaly at epoch: | 118.4500° |
| orbit number at epoch: | 43221 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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