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 48274U 21035A 22176.47654722 .00012192 00000-0 14746-3 0 9991
2 48274 41.4701 168.5170 0003574 324.4979 174.1983 15.60516824 66068
| Epoch (UTC): | 25 June 2022 11:26:13 |
| Eccentricity: | 0.0003574 |
| inclination: | 41.4701° |
| perigee height: | 384 km |
| apogee height: | 388 km |
| right ascension of ascending node: | 168.5170° |
| argument of perigee: | 324.4979° |
| revolutions per day: | 15.60516824 |
| mean anomaly at epoch: | 174.1983° |
| orbit number at epoch: | 6606 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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