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 00047U 60007C 22221.72126006 .00000178 00000-0 65230-4 0 9993
2 00047 66.6641 220.3306 0218996 90.2272 272.3927 14.42386845247623
| Epoch (UTC): | 09 August 2022 17:18:36 |
| Eccentricity: | 0.0218996 |
| inclination: | 66.6641° |
| perigee height: | 594 km |
| apogee height: | 907 km |
| right ascension of ascending node: | 220.3306° |
| argument of perigee: | 90.2272° |
| revolutions per day: | 14.42386845 |
| mean anomaly at epoch: | 272.3927° |
| orbit number at epoch: | 24762 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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