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 22220.40381285 .00000179 00000-0 65460-4 0 9995
2 00047 66.6639 223.8547 0218995 91.2275 271.3926 14.42386185247432
| Epoch (UTC): | 08 August 2022 09:41:29 |
| Eccentricity: | 0.0218995 |
| inclination: | 66.6639° |
| perigee height: | 594 km |
| apogee height: | 907 km |
| right ascension of ascending node: | 223.8547° |
| argument of perigee: | 91.2275° |
| revolutions per day: | 14.42386185 |
| mean anomaly at epoch: | 271.3926° |
| orbit number at epoch: | 24743 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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