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 22225.13499029 .00001492 00000-0 17951-3 0 9992
2 40074 98.3755 108.7544 0005392 96.8263 263.3562 14.85562420438487
| Epoch (UTC): | 13 August 2022 03:14:23 |
| Eccentricity: | 0.0005392 |
| inclination: | 98.3755° |
| perigee height: | 608 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 108.7544° |
| argument of perigee: | 96.8263° |
| revolutions per day: | 14.85562420 |
| mean anomaly at epoch: | 263.3562° |
| orbit number at epoch: | 43848 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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