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 27432U 02024C 22145.11163789 .00000051 00000-0 50395-4 0 9998
2 27432 99.0629 169.8881 0050086 343.8182 84.4099 14.14139396 33601
| Epoch (UTC): | 25 May 2022 02:40:45 |
| Eccentricity: | 0.0050086 |
| inclination: | 99.0629° |
| perigee height: | 809 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 169.8881° |
| argument of perigee: | 343.8182° |
| revolutions per day: | 14.14139396 |
| mean anomaly at epoch: | 84.4099° |
| orbit number at epoch: | 3360 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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